EP3279353B1 - Hot-rolled steel sheet and method for producing same - Google Patents
Hot-rolled steel sheet and method for producing same Download PDFInfo
- Publication number
- EP3279353B1 EP3279353B1 EP16771783.4A EP16771783A EP3279353B1 EP 3279353 B1 EP3279353 B1 EP 3279353B1 EP 16771783 A EP16771783 A EP 16771783A EP 3279353 B1 EP3279353 B1 EP 3279353B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- less
- steel sheet
- phase
- temperature
- content
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
- 229910000831 Steel Inorganic materials 0.000 title claims description 241
- 239000010959 steel Substances 0.000 title claims description 241
- 238000004519 manufacturing process Methods 0.000 title claims description 22
- 150000001247 metal acetylides Chemical class 0.000 claims description 68
- 229910001563 bainite Inorganic materials 0.000 claims description 60
- 229910000734 martensite Inorganic materials 0.000 claims description 60
- 238000001816 cooling Methods 0.000 claims description 41
- 238000000137 annealing Methods 0.000 claims description 36
- 238000010438 heat treatment Methods 0.000 claims description 34
- 229910001566 austenite Inorganic materials 0.000 claims description 30
- 238000005098 hot rolling Methods 0.000 claims description 29
- 229910001562 pearlite Inorganic materials 0.000 claims description 23
- 238000005096 rolling process Methods 0.000 claims description 23
- 230000000717 retained effect Effects 0.000 claims description 17
- 239000002245 particle Substances 0.000 claims description 16
- 239000002994 raw material Substances 0.000 claims description 16
- 239000000203 mixture Substances 0.000 claims description 11
- 229910052758 niobium Inorganic materials 0.000 claims description 9
- 229910052750 molybdenum Inorganic materials 0.000 claims description 8
- 229910052799 carbon Inorganic materials 0.000 claims description 6
- 229910052748 manganese Inorganic materials 0.000 claims description 5
- 229910052710 silicon Inorganic materials 0.000 claims description 5
- 229910052782 aluminium Inorganic materials 0.000 claims description 4
- 239000011248 coating agent Substances 0.000 claims description 4
- 238000000576 coating method Methods 0.000 claims description 4
- 229910052725 zinc Inorganic materials 0.000 claims description 4
- 239000012535 impurity Substances 0.000 claims description 3
- 238000005554 pickling Methods 0.000 claims description 3
- 238000007747 plating Methods 0.000 claims description 3
- 229910052718 tin Inorganic materials 0.000 claims description 3
- 229910052787 antimony Inorganic materials 0.000 claims description 2
- 229910052785 arsenic Inorganic materials 0.000 claims description 2
- 229910052792 caesium Inorganic materials 0.000 claims description 2
- 229910052791 calcium Inorganic materials 0.000 claims description 2
- 229910052804 chromium Inorganic materials 0.000 claims description 2
- 229910052802 copper Inorganic materials 0.000 claims description 2
- 229910052745 lead Inorganic materials 0.000 claims description 2
- 229910052749 magnesium Inorganic materials 0.000 claims description 2
- 229910052759 nickel Inorganic materials 0.000 claims description 2
- 229910052761 rare earth metal Inorganic materials 0.000 claims description 2
- 229910052711 selenium Inorganic materials 0.000 claims description 2
- 229910052715 tantalum Inorganic materials 0.000 claims description 2
- 229910052721 tungsten Inorganic materials 0.000 claims description 2
- 229910052726 zirconium Inorganic materials 0.000 claims description 2
- 229910052757 nitrogen Inorganic materials 0.000 claims 1
- 229910052698 phosphorus Inorganic materials 0.000 claims 1
- 229910052717 sulfur Inorganic materials 0.000 claims 1
- XEEYBQQBJWHFJM-UHFFFAOYSA-N iron Substances [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 29
- 230000007423 decrease Effects 0.000 description 24
- 230000000694 effects Effects 0.000 description 21
- 230000000052 comparative effect Effects 0.000 description 18
- 238000012360 testing method Methods 0.000 description 16
- 238000000034 method Methods 0.000 description 13
- 238000005728 strengthening Methods 0.000 description 12
- 229910000859 α-Fe Inorganic materials 0.000 description 12
- 238000001556 precipitation Methods 0.000 description 9
- 230000015572 biosynthetic process Effects 0.000 description 8
- 239000000463 material Substances 0.000 description 8
- 229910052719 titanium Inorganic materials 0.000 description 8
- 239000002244 precipitate Substances 0.000 description 7
- 229910052720 vanadium Inorganic materials 0.000 description 7
- MUBZPKHOEPUJKR-UHFFFAOYSA-N Oxalic acid Chemical compound OC(=O)C(O)=O MUBZPKHOEPUJKR-UHFFFAOYSA-N 0.000 description 6
- 238000009628 steelmaking Methods 0.000 description 6
- 238000005496 tempering Methods 0.000 description 6
- 238000009864 tensile test Methods 0.000 description 6
- 230000009466 transformation Effects 0.000 description 6
- 230000014509 gene expression Effects 0.000 description 5
- 239000011800 void material Substances 0.000 description 5
- 230000008034 disappearance Effects 0.000 description 4
- 239000000126 substance Substances 0.000 description 4
- 239000011701 zinc Substances 0.000 description 4
- 238000009749 continuous casting Methods 0.000 description 3
- 238000001739 density measurement Methods 0.000 description 3
- 230000005764 inhibitory process Effects 0.000 description 3
- 238000001000 micrograph Methods 0.000 description 3
- 230000001376 precipitating effect Effects 0.000 description 3
- 238000010791 quenching Methods 0.000 description 3
- 238000011084 recovery Methods 0.000 description 3
- 238000007670 refining Methods 0.000 description 3
- 238000005204 segregation Methods 0.000 description 3
- 239000000725 suspension Substances 0.000 description 3
- 229910001335 Galvanized steel Inorganic materials 0.000 description 2
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 description 2
- 238000005275 alloying Methods 0.000 description 2
- 238000005266 casting Methods 0.000 description 2
- 238000010276 construction Methods 0.000 description 2
- 238000005336 cracking Methods 0.000 description 2
- 239000013078 crystal Substances 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 238000011156 evaluation Methods 0.000 description 2
- 239000008397 galvanized steel Substances 0.000 description 2
- 238000000227 grinding Methods 0.000 description 2
- 238000005259 measurement Methods 0.000 description 2
- 235000006408 oxalic acid Nutrition 0.000 description 2
- 238000005498 polishing Methods 0.000 description 2
- 238000003825 pressing Methods 0.000 description 2
- SXAMGRAIZSSWIH-UHFFFAOYSA-N 2-[3-[2-(2,3-dihydro-1H-inden-2-ylamino)pyrimidin-5-yl]-1,2,4-oxadiazol-5-yl]-1-(2,4,6,7-tetrahydrotriazolo[4,5-c]pyridin-5-yl)ethanone Chemical compound C1C(CC2=CC=CC=C12)NC1=NC=C(C=N1)C1=NOC(=N1)CC(=O)N1CC2=C(CC1)NN=N2 SXAMGRAIZSSWIH-UHFFFAOYSA-N 0.000 description 1
- VPSXHKGJZJCWLV-UHFFFAOYSA-N 2-[4-[2-(2,3-dihydro-1H-inden-2-ylamino)pyrimidin-5-yl]-3-(1-ethylpiperidin-4-yl)oxypyrazol-1-yl]-1-(2,4,6,7-tetrahydrotriazolo[4,5-c]pyridin-5-yl)ethanone Chemical compound C1C(CC2=CC=CC=C12)NC1=NC=C(C=N1)C=1C(=NN(C=1)CC(=O)N1CC2=C(CC1)NN=N2)OC1CCN(CC1)CC VPSXHKGJZJCWLV-UHFFFAOYSA-N 0.000 description 1
- DXCXWVLIDGPHEA-UHFFFAOYSA-N 2-[4-[2-(2,3-dihydro-1H-inden-2-ylamino)pyrimidin-5-yl]-3-[(4-ethylpiperazin-1-yl)methyl]pyrazol-1-yl]-1-(2,4,6,7-tetrahydrotriazolo[4,5-c]pyridin-5-yl)ethanone Chemical compound C1C(CC2=CC=CC=C12)NC1=NC=C(C=N1)C=1C(=NN(C=1)CC(=O)N1CC2=C(CC1)NN=N2)CN1CCN(CC1)CC DXCXWVLIDGPHEA-UHFFFAOYSA-N 0.000 description 1
- APLNAFMUEHKRLM-UHFFFAOYSA-N 2-[5-[2-(2,3-dihydro-1H-inden-2-ylamino)pyrimidin-5-yl]-1,3,4-oxadiazol-2-yl]-1-(3,4,6,7-tetrahydroimidazo[4,5-c]pyridin-5-yl)ethanone Chemical compound C1C(CC2=CC=CC=C12)NC1=NC=C(C=N1)C1=NN=C(O1)CC(=O)N1CC2=C(CC1)N=CN2 APLNAFMUEHKRLM-UHFFFAOYSA-N 0.000 description 1
- YLZOPXRUQYQQID-UHFFFAOYSA-N 3-(2,4,6,7-tetrahydrotriazolo[4,5-c]pyridin-5-yl)-1-[4-[2-[[3-(trifluoromethoxy)phenyl]methylamino]pyrimidin-5-yl]piperazin-1-yl]propan-1-one Chemical compound N1N=NC=2CN(CCC=21)CCC(=O)N1CCN(CC1)C=1C=NC(=NC=1)NCC1=CC(=CC=C1)OC(F)(F)F YLZOPXRUQYQQID-UHFFFAOYSA-N 0.000 description 1
- 229910000838 Al alloy Inorganic materials 0.000 description 1
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 229910001208 Crucible steel Inorganic materials 0.000 description 1
- 238000003917 TEM image Methods 0.000 description 1
- -1 TiC Chemical class 0.000 description 1
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 description 1
- 229910045601 alloy Inorganic materials 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- JZQOJFLIJNRDHK-CMDGGOBGSA-N alpha-irone Chemical compound CC1CC=C(C)C(\C=C\C(C)=O)C1(C)C JZQOJFLIJNRDHK-CMDGGOBGSA-N 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- ZDVYABSQRRRIOJ-UHFFFAOYSA-N boron;iron Chemical group [Fe]#B ZDVYABSQRRRIOJ-UHFFFAOYSA-N 0.000 description 1
- 229910001567 cementite Inorganic materials 0.000 description 1
- 239000012141 concentrate Substances 0.000 description 1
- 238000007796 conventional method Methods 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 230000001934 delay Effects 0.000 description 1
- 238000006477 desulfuration reaction Methods 0.000 description 1
- 230000023556 desulfurization Effects 0.000 description 1
- 238000003618 dip coating Methods 0.000 description 1
- 230000001747 exhibiting effect Effects 0.000 description 1
- 230000002349 favourable effect Effects 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 238000005246 galvanizing Methods 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- KSOKAHYVTMZFBJ-UHFFFAOYSA-N iron;methane Chemical compound C.[Fe].[Fe].[Fe] KSOKAHYVTMZFBJ-UHFFFAOYSA-N 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 230000003647 oxidation Effects 0.000 description 1
- 238000007254 oxidation reaction Methods 0.000 description 1
- 238000003303 reheating Methods 0.000 description 1
- 238000012827 research and development Methods 0.000 description 1
- 238000001878 scanning electron micrograph Methods 0.000 description 1
- 239000006104 solid solution Substances 0.000 description 1
- 239000000243 solution Substances 0.000 description 1
- 238000010998 test method Methods 0.000 description 1
- 239000010409 thin film Substances 0.000 description 1
Images
Classifications
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
- 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
- C21D1/00—General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
- C21D1/18—Hardening; Quenching with or without subsequent tempering
- C21D1/25—Hardening, combined with annealing between 300 degrees Celsius and 600 degrees Celsius, i.e. heat refining ("Vergüten")
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D6/00—Heat treatment of ferrous alloys
- C21D6/005—Heat treatment of ferrous alloys containing Mn
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D6/00—Heat treatment of ferrous alloys
- C21D6/008—Heat treatment of ferrous alloys containing Si
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D6/00—Heat treatment of ferrous alloys
- C21D6/02—Hardening by precipitation
-
- 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
- C21D9/00—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
- C21D9/46—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for sheet metals
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/001—Ferrous alloys, e.g. steel alloys containing N
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/002—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
- C22C38/08—Ferrous alloys, e.g. steel alloys containing nickel
-
- 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
- C22C38/10—Ferrous alloys, e.g. steel alloys containing cobalt
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/12—Ferrous alloys, e.g. steel alloys containing tungsten, tantalum, molybdenum, vanadium, or niobium
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/14—Ferrous alloys, e.g. steel alloys containing 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
- C22C38/16—Ferrous alloys, e.g. steel alloys containing copper
-
- 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
- C22C38/28—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
- C22C38/38—Ferrous alloys, e.g. steel alloys containing chromium with more than 1.5% by weight of 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
- C22C38/60—Ferrous alloys, e.g. steel alloys containing lead, selenium, tellurium, or antimony, or more than 0.04% by weight of sulfur
-
- 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
-
- 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
- C21D2211/004—Dispersions; Precipitations
-
- 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
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
- C21D8/0247—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the heat treatment
- C21D8/0273—Final recrystallisation annealing
Definitions
- the disclosure relates to a hot rolled steel sheet having high strength such as a tensile strength (TS) of 780 MPa or more, excellent stretch flangeability and blanking workability, and excellent manufacturing stability and suitable for structural-use steel material such as material for parts of transport machinery including vehicles and construction steel material.
- TS tensile strength
- the disclosure also relates to a method of manufacturing the hot rolled steel sheet.
- An effective way of lightening automotive bodies while maintaining their strength is to strengthen steel sheets as material for automotive parts to thus reduce the thickness of steel sheets.
- automotive suspension parts in which thick steel sheets tend to be used are expected to be lightened considerably by reducing the thickness of steel sheets through strengthening.
- automotive suspension parts such as lower control arms are formed by burring, and so require steel sheets to have excellent stretch flangeability.
- Much research and development have been conducted for hot rolled steel sheets having both strength and workability, and various techniques have been proposed. For example, it is known that high tensile strength and excellent stretch flangeability can both be achieved by making the metallic microstructure a substantially ferrite single-phase microstructure and precipitating fine carbides in the grains of the ferrite phase.
- JP 2012-26034 A discloses a hot rolled steel sheet whose strength is improved while maintaining stretch flangeability, by making the steel sheet microstructure a ferrite single-phase microstructure having excellent workability with low dislocation density and dispersing and precipitating fine carbides in the ferrite to achieve strengthening by precipitation.
- Burring is typically performed using a steel sheet blanked in a predetermined shape.
- the part blanking clearance usually varies due to a temperature increase or wear of the tool caused by continuous pressing.
- defects such as cracking or chipping may occur in the punched end surface. This has raised demand for a steel sheet that maintains excellent blanking workability regardless of the variations of the blanking conditions.
- JP 2014-205888 A discloses a high strength hot rolled steel sheet whose mass-production blanking workability is improved by setting the volume fraction of bainite phase to more than 92%, setting the average spacing of bainite laths to 0.60 ⁇ m or less, and setting the number ratio of Fe-based carbides precipitated in the grains to all Fe-based carbides to 10% or more.
- WO 2014/171062 A1 discloses a high strength hot rolled steel sheet with a microstructure mainly composed of a bainite phase, the bainite having an average lath interval of 0.45 ⁇ m or less.
- the steel sheet described in PTL 1 has both high strength and excellent stretch flangeability.
- the steel sheet microstructure is a substantially ferrite single-phase microstructure, there is hardly any inclusion that serves as a void origin when blanking the steel sheet. Accordingly, in the steel sheet described in PTL 1, the punched end surface may become rough when conditions such as clearance and a blank holder vary.
- the steel sheet described in PTL 2 has excellent blanking workability, by controlling the hot rolling conditions so that the steel sheet microstructure is mainly composed of predetermined bainite.
- a bainite microstructure tends to vary in mechanical properties such as tensile strength due to variations in coiling temperature. It is often not easy to keep uniform steel sheet temperature throughout the length and width of the coil during cooling after hot rolling.
- the steel sheet described in PTL 2 may thus vary greatly in mechanical properties, leading to lower manufacturing stability.
- TS tensile strength
- the steel sheet having the bainite single-phase microstructure has excellent stretch flangeability.
- the steel sheet having the bainite single-phase microstructure also has excellent blanking workability, because many Fe-based carbides are present in the bainite microstructure and serve as a void origin during blanking.
- the bainite microstructure varies greatly in mechanical properties such as strength depending on the transformation temperature, there is a possibility that the mechanical properties of the steel sheet vary greatly due to variations in hot rolling conditions such as coiling temperature.
- Tempering a bainite or martensite microstructure typically enables a significant reduction of the variations of the mechanical properties caused by the variations of the hot rolling conditions, but also leads to a significant decrease in steel sheet strength. Besides, since Fe-based carbide morphology in tempered bainite or tempered martensite phase varies depending on the annealing conditions, the steel sheet may not be able to have excellent blanking workability depending on the annealing conditions.
- the aforementioned steel sheet microstructure can be stably obtained particularly by adding 0.03% or more Ti and appropriately adjusting heat hysteresis in the annealing.
- MC-type carbides are carbides, such as TiC, NbC, VC, and (Ti, Mo)C, with an atom ratio between an M element (for example, Ti, Nb, V, or Mo) and C of approximately 1:1.
- M element for example, Ti, Nb, V, or Mo
- the M element need not be of one type, and a complex carbide containing a plurality of metal elements is applicable.
- a N-containing carbonitride or complex carbonitride is applicable, too.
- a hot rolled steel sheet that has high strength such as a tensile strength (TS) of 780 MPa or more and excellent stretch flangeability and blanking workability and whose variations in mechanical properties caused by variations in manufacturing conditions are reduced, which is suitable for structural-use steel material such as material for parts of transport machinery including vehicles and construction steel material.
- TS tensile strength
- FIG. 1 is a schematic diagram illustrating an example of a microstructure in which tempered bainite phase and tempered martensite phase have laths as a substructure and Fe-based carbides precipitate and MC-type carbides disperse and precipitate inside and at the boundaries of the laths.
- the C content improves the strength of the steel, and promotes the formation of bainite and martensite during hot rolling.
- the C content therefore needs to be 0.03% or more. If the C content is more than 0.20%, equivalent carbon content is excessively high, which causes a decrease in weldability of the steel sheet.
- the C content is therefore 0.03% or more and 0.20% or less.
- the C content is preferably 0.04% or more.
- the C content is preferably 0.18% or less.
- the C content is more preferably more than 0.05%.
- the C content is more preferably 0.15% or less.
- Si is actively used in a high strength steel sheet as an effective element that improves the steel sheet strength without decreasing ductility (elongation). If the Si content is more than 0.4%, however, Si forms oxides on the steel sheet surface during heat treatment, and degrades coating adhesion property. The Si content is therefore 0.4% or less. The Si content is preferably 0.3% or less. The Si content is more preferably 0.2% or less. The Si content may be reduced to an impurity level, and may be 0%.
- Mn 0.5% or more and 2.0% or less
- Mn is an element that dissolves and contributes to higher strength of the steel. Mn also promotes the formation of bainite and martensite during hot rolling, by improving quench hardenability. To achieve such effects, the Mn content needs to be 0.5% or more. If the Mn content is more than 2.0%, austenite becomes excessively stable, causing the microstructure of the steel sheet to excessively contain martensite and retained austenite. This decreases stretch flangeability. The Mn content is therefore 0.5% or more and 2.0% or less. The Mn content is preferably 0.8% or more. The Mn content is preferably 1.8% or less. The Mn content is more preferably 1.0% or more. The Mn content is more preferably 1.7% or less.
- P is a harmful element that segregates to grain boundaries to decrease elongation, induce cracking during working, and degrade anti-crash property.
- the P content is therefore 0.03% or less. Excessive dephosphorization, however, leads to longer refining time and higher cost, and so the P content is preferably 0.002% or more.
- S exists as MnS or TiS in the steel, and facilitates the formation of voids when blanking the hot rolled steel sheet. S also serves as a void origin during working, and causes a decrease in stretch flangeability.
- the S content is therefore desirably as low as possible, and is 0.03% or less.
- the S content is preferably 0.01% or less. Excessive desulfurization, however, leads to longer refining time and higher cost, and so the S content is preferably 0.0002% or more.
- Al is an element that acts as a deoxidizing material.
- the Al content is desirably 0.01% or more. If the Al content is more than 0.1%, Al remains in the steel sheet as Al oxide. Such Al oxide tends to coagulate and be coarsened, causing a decrease in stretch flangeability.
- the Al content is therefore 0.1% or less.
- N exists as coarse TiN in the steel, and facilitates the formation of coarse voids when blanking the hot rolled steel sheet. N also serves as an origin of coarse voids during working, and causes a decrease in stretch flangeability.
- the N content is therefore desirably as low as possible, and is 0.01% or less.
- the N content is preferably 0.006% or less. Excessive denitrification, however, leads to longer refining time and higher cost, and so the N content is preferably 0.0005% or more.
- Ti is a necessary element to form MC-type carbides to thus inhibit lath coarsening in the annealing and strengthen the steel sheet.
- MC-type carbides also enhance the steel sheet strength by strengthening by precipitation. If the Ti content is less than 0.03%, such effects are insufficient, and lath coarsening and lower precipitation amount cause a decrease in steel sheet strength, making it difficult to achieve desired steel sheet strength (tensile strength of 780 MPa or more). If the Ti content is more than 0.15%, central segregation is noticeable, causing a decrease in blanking workability.
- the Ti content is therefore 0.03% or more and 0.15% or less.
- the Ti content is preferably 0.04% or more.
- the Ti content is preferably 0.14% or less.
- the Ti content is further preferably 0.05% or more.
- the Ti content is further preferably 0.13% or less.
- the hot rolled steel sheet may optionally contain one or more of V: 0.01% or more and 0.3% or less, Nb: 0.01% or more and 0.1 % or less, and Mo: 0.01% or more and 0.3% or less, for higher strength.
- V 0.01% or more and 0.3% or less
- V forms MC-type carbides and contributes to higher strength of the steel sheet by lath coarsening inhibition in the annealing and strengthening by precipitation, as with Ti. To achieve such effects, the V content needs to be 0.01% or more. If the V content is more than 0.3%, central segregation is noticeable, causing a decrease in blanking workability. Accordingly, the V content is preferably 0.01% or more. The V content is preferably 0.3% or less. The V content is more preferably 0.01% or more. The V content is more preferably 0.2% or less. The V content is further preferably 0.01% or more. The V content is further preferably 0.15% or less. V may form MC-type carbides by itself, or form complex carbides with Ti, Nb, and Mo. Such carbide composition does not affect the advantageous effects of the disclosure at all.
- Nb 0.01% or more and 0.1% or less
- Nb forms MC-type carbides and contributes to higher strength of the steel sheet by lath coarsening inhibition in the annealing and strengthening by precipitation, as with Ti.
- the Nb content needs to be 0.01% or more. If Nb is excessively added to be more than 0.1% in content, Nb does not dissolve in the heating furnace during hot rolling. The effects thus saturate, and the alloy cost increases. Accordingly, the Nb content is preferably 0.01% or more.
- the Nb content is preferably 0.1% or less.
- the Nb content is more preferably 0.01% or more.
- the Nb content is more preferably 0.08% or less.
- the Nb content is further preferably 0.01% or more.
- the Nb content is further preferably 0.06% or less.
- Nb may form MC-type carbides by itself, or form complex carbides with Ti, V, and Mo. Such carbide composition does not affect the advantageous effects of the disclosure at all.
- Mo when added in combination with Ti, forms MC-type complex carbides and contributes to higher strength of the steel sheet by lath coarsening inhibition in the annealing and strengthening by precipitation, as with Ti.
- the Mo content needs to be 0.01% or more. If the Mo content is more than 0.3%, central segregation is noticeable, causing a decrease in blanking workability. Accordingly, the Mo content is preferably 0.01% or more. The Mo content is preferably 0.3% or less. Mo may form complex carbides with Nb and V. Such carbide composition does not affect the advantageous effects of the disclosure at all.
- the hot rolled steel sheet may optionally contain B: 0.0002% or more and 0.010% or less, for improved quench hardenability during hot rolling.
- the B is an element that segregates to austenite grain boundaries and inhibits the formation and growth of ferrite to improve quench hardenability and promote the formation of bainite and martensite.
- the B content is preferably 0.0002% or more. If the B content is more than 0.010%, hard iron boride forms and causes a decrease in stretch flangeability. Accordingly, in the case of adding B, the B content is preferably 0.0002% or more and 0.010% or less.
- the B content is more preferably 0.0002% or more.
- the B content is more preferably 0.0050% or less.
- the B content is further preferably 0.0004% or more.
- the B content is further preferably 0.0030% or less.
- the hot rolled steel sheet may contain one or more of REM, Zr, As, Cu, Ni, Sn, Pb, Ta, W, Cr, Sb, Mg, Ca, Co, Se, Zn, and Cs so that their total content is 1.0% or less.
- the components other than those described above are Fe and incidental impurities.
- Total area ratio of tempered bainite phase and tempered martensite phase 70% or more
- the hot rolled steel sheet has a microstructure mainly composed of tempered bainite and tempered martensite having both high strength and excellent blanking workability. If the total area ratio of tempered bainite phase and tempered martensite phase is less than 70%, the hot rolled steel sheet cannot have desired high strength and blanking workability.
- the ratio of each of tempered bainite phase and tempered martensite is not individually defined because tempered bainite and tempered martensite after annealing are microstructures not distinguishable from each other. This is a major factor that can reduce variations in mechanical properties after annealing in the case where the manufacturing conditions during hot rolling vary.
- the total area ratio of tempered bainite phase and tempered martensite phase is therefore 70% or more.
- the total area ratio of tempered bainite phase and tempered martensite phase is preferably 75% or more.
- the total area ratio of tempered bainite phase and tempered martensite phase is more preferably 80% or more.
- the total area ratio of tempered bainite phase and tempered martensite phase may be 100%.
- Total area ratio of coarse pearlite phase, martensite phase, and retained austenite phase 10% or less
- the microstructure of the hot rolled steel sheet is mainly composed of tempered bainite and tempered martensite, with the balance other than tempered bainite and tempered martensite being, for example, Fe-based carbides, coarse pearlite, fine pearlite, degenerate pearlite, bainite, martensite, and retained austenite.
- tempered bainite and tempered martensite being, for example, Fe-based carbides, coarse pearlite, fine pearlite, degenerate pearlite, bainite, martensite, and retained austenite.
- the total area ratio of coarse pearlite phase, martensite phase, and retained austenite phase is therefore 10% or less.
- the total area ratio of coarse pearlite phase, martensite phase, and retained austenite phase is preferably 8% or less.
- the total area ratio of coarse pearlite phase, martensite phase, and retained austenite phase is more preferably 5% or less.
- coarse pearlite has a lamellar spacing of 0.2 ⁇ m or more
- fine pearlite has a lamellar spacing of less than 0.2 ⁇ m
- degenerate pearlite is a phase in which pearlite lamellar is not clearly observable.
- the lamellar spacing can be measured by microstructure observation using a scanning electron microscope.
- the balance other than tempered bainite phase, tempered martensite phase, coarse pearlite phase, martensite phase, and retained austenite phase is, for example, ferrite phase, degenerate pearlite phase, and fine pearlite phase.
- a total area ratio of such balance of 30% or less is allowable.
- Average width of laths which tempered bainite phase and tempered martensite phase have as substructure 1.0 ⁇ m or less
- FIG. 1 is a schematic diagram illustrating an example of a microstructure in which tempered bainite phase and tempered martensite phase have laths as their substructure and Fe-based carbides precipitate and MC-type carbides disperse and precipitate inside and at the boundaries of the laths. If the laths disappears as a result of recovery or the average width of the laths is more than 1.0 ⁇ m, predetermined high strength cannot be achieved.
- the average width of laths which tempered bainite phase and tempered martensite phase have as their substructure is therefore 1.0 ⁇ m or less.
- the average width of laths is preferably 0.8 ⁇ m or less.
- the average width of laths is more preferably 0.6 ⁇ m or less. No lower limit is placed on the average width of laths, yet the lower limit is typically about 0.1 ⁇ m.
- Fe-based carbides precipitated inside and at the boundaries of laths as illustrated in FIG. 1 serve as a void origin during blanking, thus contributing to improved blanking workability. This effect is particularly high with Fe-based carbides having an aspect ratio of 5 or less.
- the proportion of Fe-based carbides with an aspect ratio of 5 or less in Fe-based carbides precipitated inside and at the boundaries of laths is therefore 80% or more.
- the proportion is preferably 85% or more. No upper limit is placed on the proportion, yet the upper limit may be 100%.
- Fe-based carbides are ⁇ carbide (cementite), ⁇ carbide, and the like.
- An alloying element may be dissolved in the carbides.
- the aspect ratio is the ratio of the major axis length and minor axis length of Fe-based carbides precipitated inside and at the boundaries of laths.
- Average particle size of MC-type carbides dispersed and precipitated inside and at the boundaries of laths 20 nm or less
- MC-type carbides finely dispersed and precipitated inside and at the boundaries of laths as illustrated in FIG. 1 inhibit lath coarsening by a pinning effect when annealing the steel sheet and also inhibit lath disappearance resulting from recovery, thus contributing to higher strength. If the average particle size of MC-type carbides is more than 20 nm, the number of particles of MC-type carbides contributing to pinning is insufficient and so the pinning effect is insufficient, causing a decrease in steel sheet strength. If the average particle size of MC-type carbides is 20 nm or less, a sufficient number of particles of MC-type carbides exhibit the pinning effect, to prevent a decrease in steel sheet strength.
- the average particle size of MC-type carbides dispersed and precipitated inside and at the boundaries of laths of tempered bainite phase and tempered martensite phase is therefore 20 nm or less.
- the average particle size is preferably 15 nm or less. No lower limit is placed on the average particle size, yet the lower limit is typically about 1 nm.
- the proportion of MC-type carbides with a particle size of more than 50 nm is preferably 10% or less.
- the hot rolled steel sheet has an average dislocation density in the following range.
- Average dislocation density 1.0 ⁇ 10 14 m -2 or more and 5.0 ⁇ 10 15 m -2 or less
- the variations of the hot rolled steel sheet caused by the variations of the hot rolling conditions are reduced by tempering the steel sheet having bainite and martensite microstructure. If the average dislocation density of the steel sheet after annealing is more than 5.0 ⁇ 10 15 m -2 , the tempering of the steel sheet is insufficient and the influence of the variations of the hot rolling conditions cannot be reduced sufficiently. In the case where tempering is sufficient, the average dislocation density is typically 1.0 ⁇ 10 14 m -2 or more. The average dislocation density is therefore 1.0 ⁇ 10 14 m -2 or more and 5.0 ⁇ 10 15 m -2 or less. The average dislocation density is preferably 1.0 ⁇ 10 14 m -2 or more. The average dislocation density is preferably 2.0 ⁇ 10 15 m -2 or less.
- the method of manufacturing the hot rolled steel sheet includes: hot rolling a steel raw material having the chemical composition described above, whereby the steel raw material is heated to an austenite single phase region, subjected to rough rolling and finish rolling to obtain a steel sheet, and the steel sheet is cooled and coiled after the finish rolling; pickling the steel sheet after the hot rolling; and then continuous annealing the steel sheet, wherein in the hot rolling, a finisher delivery temperature is 850 °C or more and 1000 °C or less, an average cooling rate to 500 °C after the finish rolling is 30 °C/s or more, and a coiling temperature is 500 °C or less, and in the continuous annealing, a maximum heating temperature of the steel sheet is 700 °C or more and (A 3 point + A 1 point)/2 or less, a time during which a temperature of the steel sheet is 600 °C or more and 700 °C or less in heating the steel sheet to the maximum heating temperature is 20 s or more and 1000 s or less, a time during
- the method of obtaining the steel raw material by steelmaking is not limited, and any known steelmaking process such as a converter steelmaking process or an electric furnace steelmaking process may be used.
- continuous casting is preferably performed to yield a slab (steel raw material) in terms of productivity and the like.
- the slab may be yielded by a known casting method such as ingot casting and blooming, thin slab continuous casting, or the like.
- the obtained steel raw material is subjected to hot rolling, in which the steel raw material is subjected to rough rolling and finish rolling. Before the rough rolling, the steel raw material is heated in the austenite single phase region. If the steel raw material before the rough rolling is not heated in the austenite single phase region, the remelting of Ti carbide and the like present in the steel raw material does not progress, and fine MC-type carbides do not precipitate during the annealing after the hot rolling. Accordingly, the steel raw material is heated to 1150 °C or more, before the rough rolling. No upper limit is placed on the heating temperature, yet an excessively high heating temperature leads to a considerable decrease in yield rate due to the oxidation of the slab surface, and so the heating temperature is typically 1350 °C or less. In the case where the temperature of the cast steel raw material (slab) is in the austenite single phase region when hot rolling the steel raw material, the steel raw material may be subjected to hot direct rolling without being heated or after being heated for a short time.
- Finisher delivery temperature 850 °C or more and 1000 °C or less
- the finisher delivery temperature needs to be 850 °C or more.
- the finisher delivery temperature is preferably 880 °C or more. If the finisher delivery temperature is more than 1000 °C, the surface characteristics of the steel sheet degrade. The finisher delivery temperature is therefore 1000 °C or less.
- the finisher delivery temperature is preferably 970 °C or less.
- Each of the temperatures such as the finisher delivery temperature and the coiling temperature mentioned here is the temperature of the steel sheet surface.
- Cooling rate to 500 °C after finish rolling 30 °C/s or more
- the cooling rate to 500 °C after the finish rolling needs to be 30 °C/s or more.
- the cooling rate is preferably 50 °C/s or more. No upper limit is placed on the cooling rate, yet the upper limit is typically about 300 °C/s.
- Coiling temperature 500 °C or less
- the coiling temperature is important in controlling the steel sheet microstructure after the hot rolling. If the coiling temperature is more than 500 °C, the lath width of bainite increases. This makes it impossible to obtain a predetermined lath width of tempered bainite after the annealing. No lower limit is placed on the coiling temperature, yet an excessively low coiling temperature merely leads to higher cooling cost, and so the coiling temperature is preferably 0 °C or more. The coiling temperature is more preferably 200 °C or more.
- the hot rolled steel sheet After the hot rolling, the hot rolled steel sheet is subjected to pickling and then to continuous annealing.
- the reasons for limiting the manufacturing conditions in the continuous annealing are given below.
- Appropriately adjusting the maximum heating temperature of the steel sheet in the continuous annealing is important in sufficiently reducing the influence of the variations of the manufacturing conditions in the hot rolling caused by the annealing and achieving desired high strength. If the maximum heating temperature of the steel sheet is less than 700 °C, the dislocation density in bainite and martensite is difficult to be controlled within an appropriate range, and so the influence of the variations of the manufacturing conditions in the hot rolling cannot be reduced sufficiently. Besides, if the heating temperature of the steel sheet is less than 700 °C, the aspect ratio of Fe-based carbides inside and between laths tends to be high, which makes it difficult to set the proportion of Fe-based carbides with an aspect ratio of 5 or less to be in a desired range.
- the maximum heating temperature of the steel sheet in the continuous annealing is therefore 700 °C or more and (A 3 point + A 1 point)/2 or less.
- the maximum heating temperature is preferably 700 °C or more.
- the maximum heating temperature is preferably ⁇ (A 3 point + A 1 point)/2 ⁇ - 10 °C or less.
- the A 1 point and the A 3 point can be calculated according to the following expressions.
- a 1 point 751 ⁇ 26.6 ⁇ % C + 17.6 ⁇ % Si ⁇ 11.6 ⁇ % Mn + 22.5 ⁇ % Mo + 233 ⁇ % Nb ⁇ 39.7 ⁇ % V ⁇ 57 ⁇ % Ti ⁇ 895 ⁇ % B ⁇ 169 ⁇ % Al
- a 3 point 937 ⁇ 476.5 ⁇ % C + 56 ⁇ % Si ⁇ 19.7 ⁇ % Mn + 38.1 ⁇ % Mo + 124.8 ⁇ % V + 136.3 ⁇ % Ti ⁇ 19 ⁇ % Nb + 3315 ⁇ % B
- [%X] denotes the content of an X element in steel (mass%).
- MC-type carbides In heating the steel sheet to the maximum heating temperature, it is important to appropriately control heat hysteresis in imparting desired high strength and excellent blanking workability to the steel sheet.
- the pinning effect of MC-type carbides is used to inhibit lath coarsening, as mentioned above. To achieve the pinning effect, MC-type carbides need to be sufficiently dispersed in bainite and martensite before lath coarsening starts. According to our study, the precipitation of MC-type carbides begins to occur noticeably at 600 °C or more. Meanwhile, lath coarsening and disappearance are noticeable at more than 700 °C.
- lath coarsening and disappearance can be inhibited by holding the steel sheet temperature in the temperature range of 600 °C or more and 700 °C or less for a predetermined time so that MC-type carbides precipitate sufficiently.
- the holding time in this temperature range needs to be 20 s or more. If the holding time in the temperature range is insufficient, lath coarsening starts before MC-type carbides precipitate sufficiently, so that the pinning effect is insufficient and the laths coarsen.
- the holding time is preferably 35 s or more.
- the holding time is more preferably 50 s or more.
- the holding time of the steel sheet temperature in the temperature range of 600 °C or more and 700 °C or less is more than 1000 s, Fe-based carbides precipitated inside and between laths dissolve again and move to prior austenite grain boundaries, packet grain boundaries, block grain boundaries, and the like. Thus, Fe-based carbides inside and between laths that effectively contribute to improved blanking workability no longer exist. Accordingly, to obtain a steel sheet having excellent blanking workability, the holding time of the steel sheet temperature in the temperature range of 600 °C or more and 700 °C or less needs to be 1000 s or less.
- the holding time is preferably 800 s or less.
- the holding time is more preferably 500 s or less.
- the steel sheet temperature mentioned here is the temperature of the steel sheet surface.
- the holding time in this temperature range is excessively long, however, lath coarsening cannot be inhibited. Accordingly, the holding time of the steel sheet temperature in the temperature range of more than 700 °C is 200 s or less, in terms of preventing lath coarsening.
- the holding time is preferably 180 s or less.
- the holding time is more preferably 150 s or less. If the time during which the steel sheet temperature is more than 700 °C is less than 10 s, the ductility of the steel sheet decreases to some extent, and so the holding time is 10 s or more.
- Average cooling rate to 530 °C when cooling the steel sheet from the maximum heating temperature 8 °C/s or more and 25 °C/s or less
- non-transformed austenite transforms to martensite or remains in the steel sheet microstructure as retained austenite, so that stretch flangeability decreases.
- the holding time in the temperature range of 470 °C or more and 530 °C or less after the controlled cooling stops is 10 s or more.
- the holding time is preferably 20 s or more.
- the holding time is more preferably 30 s or more. No upper limit is placed on the holding time, yet the holding time is typically 300 s or less.
- Holding the steel sheet in the temperature range of 470 °C or more and 530 °C or less completes the control of the steel sheet microstructure.
- the subsequent cooling conditions are not limited, and the steel sheet may be cooled to room temperature by any cooling method.
- desired steel sheet microstructure can still be obtained as long as the total holding time in the temperature range of 600 °C or more and 700 °C or less is 1000 s or less.
- the steel sheet may be immersed in a zinc pot to yield a hot-dip galvanized steel sheet.
- the steel sheet may then be further heated to yield a galvannealed steel sheet.
- the hot dip coating is not limited to zinc, and may be a coating of aluminum, an aluminum alloy, or the like.
- the steel sheet may be subjected to temper rolling either continuously in the annealing line or using another line according to a conventional method.
- the hot rolled steel sheet manufactured as described above may be electrogalvanized or hot-dip galvanized.
- the hot rolled steel sheet according to the disclosure is suitable not only as a steel sheet for automotive suspension parts but also for press forming typically performed at ordinary temperature, and has excellent heat resistance.
- the hot rolled steel sheet manufactured as described above is also suitable as a blank sheet for a warm forming process of heating a steel sheet to 400 °C to 700 °C before pressing and then immediately press forming the steel sheet.
- Molten steels having the compositions listed in Table 1 were each obtained by steelmaking and subjected to continuous casting by a typically known technique, to yield a slab (steel raw material) with a thickness of 300 mm.
- the slab was heated to the temperature in Table 2, rough rolled, and finish rolled at the finisher delivery temperature in Table 2.
- the steel sheet was cooled at the average cooling rate in Table 2, and coiled at the coiling temperature in Table 2, to obtain a hot rolled steel sheet with a sheet thickness of 3.2 mm.
- the hot rolled steel sheet was then pickled by a typically known technique, and annealed in a continuous annealing line under the conditions in Table 2.
- test piece was collected from each obtained hot rolled steel sheet, and subjected to microstructure observation, average dislocation density measurement, a tensile test, a hole expansion test, a blanking test, and manufacturing stability evaluation.
- the evaluation results are listed in Table 3.
- the test methods are as follows.
- a test piece was collected from each obtained hot rolled steel sheet, and polished in a cross-section (L cross-section) parallel to the rolling direction of the test piece and etched by nital.
- a micrograph taken with a scanning electron microscope 1000, 3000, 5000 magnifications was used to determine the total area ratio of tempered bainite phase and tempered martensite phase, the area ratio of coarse pearlite phase, the total area ratio of martensite phase and retained austenite phase (MA), and the area ratio of phase other than these, through the use of an image analyzer. It is difficult to distinguish martensite phase and retained austenite phase from each other with a scanning electron micrograph.
- the total area ratio of coarse pearlite phase, martensite phase, and retained austenite phase is important, and accordingly the total area ratio of martensite phase and retained austenite phase (MA) was determined without distinguishing martensite phase and retained austenite phase from each other.
- a thin film made from each hot rolled steel sheet was observed using a transmission electron microscope (TEM), to measure the lath width in tempered bainite and tempered martensite and determine the proportion of Fe-based carbides with an aspect ratio of 5 or less in Fe-based carbides precipitated inside and at the boundaries of laths and the average particle size of MC-type carbides precipitated inside and at the boundaries of laths.
- TEM transmission electron microscope
- the lath width in tempered bainite and tempered martensite was measured as follows. In a transmission electron micrograph of 120 mm ⁇ 80 mm in size taken for 10 observation fields at 30000 magnifications, five straight lines orthogonal to the major axes of three or more consecutively aligned laths were drawn at intervals of 10 mm, the length of each line segment where the corresponding straight line intersects with the lath boundaries was measured, and the average length of the line segments was set as the average lath width.
- the proportion of Fe-based carbides with an aspect ratio of 5 or less in Fe-based carbides precipitated inside and at the boundaries of laths was determined as follows. In a micrograph taken at 165000 magnifications, the major axis length and the minor axis length were measured for at least 100 particles of Fe-based carbides precipitated inside and at the boundaries of laths for 5 observation fields in total, to calculate the aspect ratio. The proportion of Fe-based carbides with an aspect ratio of 5 or less was thus determined.
- the average particle size of MC-type carbides was determined as follows. In a micrograph taken at 300000 magnifications, the diameter was measured for at least 100 particles of MC-type carbides such as TiC for 5 observation fields in total, and an arithmetic average (average particle size d def ) was calculated. The lower limit of the measured particle size was 2 nm.
- a test piece was collected from each obtained hot rolled steel sheet, and the dislocation density of a 1/4 portion in sheet thickness was measured. Assuming that the dislocation density of a 1/4 portion in sheet thickness represents the average dislocation density of the steel sheet, the measurement was set as average dislocation density.
- the collected test piece was subjected to mechanical grinding and also polishing with oxalic acid for 0.1 mm, to adjust the sample so that the 1/4 portion in sheet thickness was exposed to the surface. Polishing with oxalic acid was intended to remove the layer worked by grinding.
- the strain of the steel sheet was measured by an X-ray diffractometer.
- an X-ray diffractometer With an X-ray diffractometer, the diffraction intensity of (110) plane, (211) plane, and (220) plane of ⁇ -iron in the 1/4 portion in sheet thickness was measured using CoK ⁇ rays.
- the half-value breadth of the peak value of the reflection intensity of each crystal plane was calculated from the obtained measurement chart, and the local strain ⁇ ' applied to the steel sheet was determined according to the following Expressions (1) and (2).
- ⁇ cos ⁇ / ⁇ 0.9 / D + 2 ⁇ ⁇ ′ sin ⁇ / ⁇
- ⁇ the half-value breadth of the peak value (the value corrected according to Expression (2) was used)
- ⁇ the diffraction angle
- ⁇ the wavelength of CoK ⁇ rays (0.1790 nm)
- D the crystallite size (dislocation cell, crystal grain size)
- ⁇ ' the local strain.
- ⁇ 2 ⁇ m 2 ⁇ ⁇ 0 2
- ⁇ m is the half-value breadth of the peak of the sample subjected to dislocation density measurement
- ⁇ 0 is the half-value breadth of the peak of a strain-free sample.
- JIS Z 2001 A JIS No. 5 tensile test piece (JIS Z 2001) was collected from each obtained hot rolled steel sheet so that the direction (C direction) orthogonal to the rolling direction was the tensile direction, and subjected to a tensile test in conformity with JIS Z 2241 to measure yield strength (YS), tensile strength (TS), and elongation (EI).
- a test piece (size: 100 mm ⁇ 100 mm) was collected from each obtained hot rolled steel sheet, and blanked with a hole of 10 mm ⁇ in initial diameter d 0 (clearance: 12.5% of the test piece sheet thickness).
- a hole expansion test was conducted using the test piece. In detail, a conical punch with a vertex angle of 60° was inserted into the hole of 10 mm ⁇ in initial diameter d 0 from the punch side at the time of blanking, to expand the hole.
- the diameter d (mm) of the hole when a crack ran through the steel sheet (test piece) was measured, and the hole expansion ratio ⁇ (%) was calculated according to the following expression.
- Hole expansion ratio ⁇ % d ⁇ d 0 / d 0 ⁇ 100.
- the stretch flangeability was evaluated as favorable in the case where tensile strength (TS) ⁇ ⁇ hole expansion ratio ( ⁇ ) ⁇ 0.5 was 6200 ⁇ MPa% 0.5 or more.
- test piece (size: 30 mm ⁇ 30 mm) was collected from each obtained hot rolled steel sheet, and blanked with a hole of 10 mm ⁇ in diameter d 0 (clearance: 20%, 30% of the test piece sheet thickness). After the blanking, the fracture state of the punched end surface was observed by a microscope (50 magnifications) on the whole circumference of the punch hole, to observe whether or not any crack, chip, or brittle fracture occurred. The blanking workability was evaluated as "pass” if there was no crack, chip, or brittle fracture, and "fail" otherwise.
- JIS No. 5 tensile test pieces JIS Z 2001 were optionally collected from the whole length and whole width of the hot rolled steel sheets of Examples so that the orthogonal direction (C direction) was the tensile direction.
- C direction the orthogonal direction
- TS tensile strength
- ⁇ the standard deviation of the tensile strength
- the mechanical properties of the steel sheet such as tensile strength (TS) had little variations, exhibiting excellent manufacturing stability.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Crystallography & Structural Chemistry (AREA)
- Heat Treatment Of Sheet Steel (AREA)
- Heat Treatment Of Steel (AREA)
Description
- The disclosure relates to a hot rolled steel sheet having high strength such as a tensile strength (TS) of 780 MPa or more, excellent stretch flangeability and blanking workability, and excellent manufacturing stability and suitable for structural-use steel material such as material for parts of transport machinery including vehicles and construction steel material. The disclosure also relates to a method of manufacturing the hot rolled steel sheet.
- To reduce CO2 emissions for global environment protection, an ever-present important issue for the automotive industry is to improve automotive fuel efficiency by lightening automotive bodies while maintaining the strength of automotive bodies. An effective way of lightening automotive bodies while maintaining their strength is to strengthen steel sheets as material for automotive parts to thus reduce the thickness of steel sheets. For example, automotive suspension parts in which thick steel sheets tend to be used are expected to be lightened considerably by reducing the thickness of steel sheets through strengthening.
- Typically, automotive suspension parts such as lower control arms are formed by burring, and so require steel sheets to have excellent stretch flangeability. Much research and development have been conducted for hot rolled steel sheets having both strength and workability, and various techniques have been proposed. For example, it is known that high tensile strength and excellent stretch flangeability can both be achieved by making the metallic microstructure a substantially ferrite single-phase microstructure and precipitating fine carbides in the grains of the ferrite phase.
- As such a technique,
JP 2012-26034 A - Burring is typically performed using a steel sheet blanked in a predetermined shape. In actual mass production of parts, the part blanking clearance usually varies due to a temperature increase or wear of the tool caused by continuous pressing. In the case where the clearance varies, defects such as cracking or chipping may occur in the punched end surface. This has raised demand for a steel sheet that maintains excellent blanking workability regardless of the variations of the blanking conditions.
- As such a steel sheet, for example,
JP 2014-205888 A - Furthermore,
WO 2014/171062 A1 (PTL 3) discloses a high strength hot rolled steel sheet with a microstructure mainly composed of a bainite phase, the bainite having an average lath interval of 0.45 µm or less. -
- PTL 1:
JP 2012-26034 A - PTL 2:
JP 2014-205888 A - PTL 3:
WO 2014/171062 A1 - The steel sheet described in PTL 1 has both high strength and excellent stretch flangeability. However, since the steel sheet microstructure is a substantially ferrite single-phase microstructure, there is hardly any inclusion that serves as a void origin when blanking the steel sheet. Accordingly, in the steel sheet described in PTL 1, the punched end surface may become rough when conditions such as clearance and a blank holder vary.
- The steel sheet described in PTL 2 has excellent blanking workability, by controlling the hot rolling conditions so that the steel sheet microstructure is mainly composed of predetermined bainite. Such a bainite microstructure, however, tends to vary in mechanical properties such as tensile strength due to variations in coiling temperature. It is often not easy to keep uniform steel sheet temperature throughout the length and width of the coil during cooling after hot rolling. The steel sheet described in PTL 2 may thus vary greatly in mechanical properties, leading to lower manufacturing stability.
- It could be helpful to provide a hot rolled steel sheet having high strength such as a tensile strength (TS) of 780 MPa or more, excellent stretch flangeability and blanking workability, and excellent manufacturing stability, together with an advantageous method of manufacturing the hot rolled steel sheet.
- We carefully examined a method that can strengthen a steel sheet while maintaining workability and especially stretch flangeability, provide excellent blanking workability, and reduce variations in mechanical properties caused by variations in manufacturing conditions.
- To improve the stretch flangeability of a steel sheet, it is effective to uniformize the strength in the metallic microstructure, as mentioned above. Available techniques include a strengthening technique of forming a ferrite single-phase microstructure to achieve solid solution strengthening or strengthening by precipitation and a strengthening technique of forming a bainite single-phase microstructure to achieve microstructure strengthening. However, in the steel sheet having the ferrite single-phase microstructure, there is hardly any inclusion that serves as a void origin when blanking the steel sheet, so that the punched end surface may become rough when conditions such as clearance and a blank holder vary.
- The steel sheet having the bainite single-phase microstructure has excellent stretch flangeability. The steel sheet having the bainite single-phase microstructure also has excellent blanking workability, because many Fe-based carbides are present in the bainite microstructure and serve as a void origin during blanking. However, since the bainite microstructure varies greatly in mechanical properties such as strength depending on the transformation temperature, there is a possibility that the mechanical properties of the steel sheet vary greatly due to variations in hot rolling conditions such as coiling temperature.
- We then considered reducing the influence of the variations of the hot rolling conditions by tempering a microstructure mainly composed of bainite or bainite and martensite.
- Tempering a bainite or martensite microstructure typically enables a significant reduction of the variations of the mechanical properties caused by the variations of the hot rolling conditions, but also leads to a significant decrease in steel sheet strength. Besides, since Fe-based carbide morphology in tempered bainite or tempered martensite phase varies depending on the annealing conditions, the steel sheet may not be able to have excellent blanking workability depending on the annealing conditions.
- In view of this, we carefully examined a technique of preventing such a decrease in steel sheet strength and achieving excellent stretch flangeability and blanking workability when tempering the microstructure mainly composed of bainite or bainite and martensite.
- We consequently discovered that dispersing and precipitating MC-type carbides such as TiC inside and at the boundaries of laths inhibits the coarsening of laths during annealing and the disappearance of laths resulting from recovery, so that high steel sheet strength can be maintained even after annealing. We also discovered that excellent blanking workability is achieved by ensuring that Fe-based carbides with an aspect ratio of 5 or less make up at least a predetermined proportion in Fe-based carbides precipitated inside and at the boundaries of laths.
- Upon further examination, we discovered that the aforementioned steel sheet microstructure can be stably obtained particularly by adding 0.03% or more Ti and appropriately adjusting heat hysteresis in the annealing.
- MC-type carbides are carbides, such as TiC, NbC, VC, and (Ti, Mo)C, with an atom ratio between an M element (for example, Ti, Nb, V, or Mo) and C of approximately 1:1. The M element need not be of one type, and a complex carbide containing a plurality of metal elements is applicable. A N-containing carbonitride or complex carbonitride is applicable, too.
- Upon further examination, we also discovered that, by appropriately controlling heat hysteresis when cooling the steel sheet from the maximum heating temperature to the room temperature in the annealing, the formation of the balance other than tempered martensite phase and tempered bainite phase, especially the formation of martensite phase, coarse pearlite phase, and retained austenite phase, is suppressed, as a result of which excellent stretch flangeability can be achieved in addition to high strength and excellent blanking workability.
- The disclosure is based on these discoveries and further studies.
- We thus provide:
A hot rolled steel sheet according to claims 1 and 2, and a method of manufacturing a hot rolled steel sheet according to claims 3 and 4. - It is possible to obtain a hot rolled steel sheet that has high strength such as a tensile strength (TS) of 780 MPa or more and excellent stretch flangeability and blanking workability and whose variations in mechanical properties caused by variations in manufacturing conditions are reduced, which is suitable for structural-use steel material such as material for parts of transport machinery including vehicles and construction steel material. This widens the range of uses of hot rolled steel sheets, and has an industrially significant advantageous effect.
- In the accompanying drawings:
FIG. 1 is a schematic diagram illustrating an example of a microstructure in which tempered bainite phase and tempered martensite phase have laths as a substructure and Fe-based carbides precipitate and MC-type carbides disperse and precipitate inside and at the boundaries of the laths. - The chemical composition of a hot rolled steel sheet according to the disclosure is described first. The unit of the content of each element in the chemical composition is "mass%", which is simply expressed as "%" below unless otherwise noted.
- C improves the strength of the steel, and promotes the formation of bainite and martensite during hot rolling. The C content therefore needs to be 0.03% or more. If the C content is more than 0.20%, equivalent carbon content is excessively high, which causes a decrease in weldability of the steel sheet. The C content is therefore 0.03% or more and 0.20% or less. The C content is preferably 0.04% or more. The C content is preferably 0.18% or less. The C content is more preferably more than 0.05%. The C content is more preferably 0.15% or less.
- Typically, Si is actively used in a high strength steel sheet as an effective element that improves the steel sheet strength without decreasing ductility (elongation). If the Si content is more than 0.4%, however, Si forms oxides on the steel sheet surface during heat treatment, and degrades coating adhesion property. The Si content is therefore 0.4% or less. The Si content is preferably 0.3% or less. The Si content is more preferably 0.2% or less. The Si content may be reduced to an impurity level, and may be 0%.
- Mn is an element that dissolves and contributes to higher strength of the steel. Mn also promotes the formation of bainite and martensite during hot rolling, by improving quench hardenability. To achieve such effects, the Mn content needs to be 0.5% or more. If the Mn content is more than 2.0%, austenite becomes excessively stable, causing the microstructure of the steel sheet to excessively contain martensite and retained austenite. This decreases stretch flangeability. The Mn content is therefore 0.5% or more and 2.0% or less. The Mn content is preferably 0.8% or more. The Mn content is preferably 1.8% or less. The Mn content is more preferably 1.0% or more. The Mn content is more preferably 1.7% or less.
- P is a harmful element that segregates to grain boundaries to decrease elongation, induce cracking during working, and degrade anti-crash property. The P content is therefore 0.03% or less. Excessive dephosphorization, however, leads to longer refining time and higher cost, and so the P content is preferably 0.002% or more.
- S exists as MnS or TiS in the steel, and facilitates the formation of voids when blanking the hot rolled steel sheet. S also serves as a void origin during working, and causes a decrease in stretch flangeability. The S content is therefore desirably as low as possible, and is 0.03% or less. The S content is preferably 0.01% or less. Excessive desulfurization, however, leads to longer refining time and higher cost, and so the S content is preferably 0.0002% or more.
- Al is an element that acts as a deoxidizing material. To achieve such effects, the Al content is desirably 0.01% or more. If the Al content is more than 0.1%, Al remains in the steel sheet as Al oxide. Such Al oxide tends to coagulate and be coarsened, causing a decrease in stretch flangeability. The Al content is therefore 0.1% or less.
- N exists as coarse TiN in the steel, and facilitates the formation of coarse voids when blanking the hot rolled steel sheet. N also serves as an origin of coarse voids during working, and causes a decrease in stretch flangeability. The N content is therefore desirably as low as possible, and is 0.01% or less. The N content is preferably 0.006% or less. Excessive denitrification, however, leads to longer refining time and higher cost, and so the N content is preferably 0.0005% or more.
- Ti is a necessary element to form MC-type carbides to thus inhibit lath coarsening in the annealing and strengthen the steel sheet. MC-type carbides also enhance the steel sheet strength by strengthening by precipitation. If the Ti content is less than 0.03%, such effects are insufficient, and lath coarsening and lower precipitation amount cause a decrease in steel sheet strength, making it difficult to achieve desired steel sheet strength (tensile strength of 780 MPa or more). If the Ti content is more than 0.15%, central segregation is noticeable, causing a decrease in blanking workability. The Ti content is therefore 0.03% or more and 0.15% or less. The Ti content is preferably 0.04% or more. The Ti content is preferably 0.14% or less. The Ti content is further preferably 0.05% or more. The Ti content is further preferably 0.13% or less.
- While the basic components have been described above, the hot rolled steel sheet may optionally contain one or more of V: 0.01% or more and 0.3% or less, Nb: 0.01% or more and 0.1 % or less, and Mo: 0.01% or more and 0.3% or less, for higher strength.
- V forms MC-type carbides and contributes to higher strength of the steel sheet by lath coarsening inhibition in the annealing and strengthening by precipitation, as with Ti. To achieve such effects, the V content needs to be 0.01% or more. If the V content is more than 0.3%, central segregation is noticeable, causing a decrease in blanking workability. Accordingly, the V content is preferably 0.01% or more. The V content is preferably 0.3% or less. The V content is more preferably 0.01% or more. The V content is more preferably 0.2% or less. The V content is further preferably 0.01% or more. The V content is further preferably 0.15% or less. V may form MC-type carbides by itself, or form complex carbides with Ti, Nb, and Mo. Such carbide composition does not affect the advantageous effects of the disclosure at all.
- Nb forms MC-type carbides and contributes to higher strength of the steel sheet by lath coarsening inhibition in the annealing and strengthening by precipitation, as with Ti. To achieve such effects, the Nb content needs to be 0.01% or more. If Nb is excessively added to be more than 0.1% in content, Nb does not dissolve in the heating furnace during hot rolling. The effects thus saturate, and the alloy cost increases. Accordingly, the Nb content is preferably 0.01% or more. The Nb content is preferably 0.1% or less. The Nb content is more preferably 0.01% or more. The Nb content is more preferably 0.08% or less. The Nb content is further preferably 0.01% or more. The Nb content is further preferably 0.06% or less. Nb may form MC-type carbides by itself, or form complex carbides with Ti, V, and Mo. Such carbide composition does not affect the advantageous effects of the disclosure at all.
- Mo, when added in combination with Ti, forms MC-type complex carbides and contributes to higher strength of the steel sheet by lath coarsening inhibition in the annealing and strengthening by precipitation, as with Ti. To achieve such effects, the Mo content needs to be 0.01% or more. If the Mo content is more than 0.3%, central segregation is noticeable, causing a decrease in blanking workability. Accordingly, the Mo content is preferably 0.01% or more. The Mo content is preferably 0.3% or less. Mo may form complex carbides with Nb and V. Such carbide composition does not affect the advantageous effects of the disclosure at all.
- The hot rolled steel sheet may optionally contain B: 0.0002% or more and 0.010% or less, for improved quench hardenability during hot rolling.
- B is an element that segregates to austenite grain boundaries and inhibits the formation and growth of ferrite to improve quench hardenability and promote the formation of bainite and martensite. To achieve such effects, the B content is preferably 0.0002% or more. If the B content is more than 0.010%, hard iron boride forms and causes a decrease in stretch flangeability. Accordingly, in the case of adding B, the B content is preferably 0.0002% or more and 0.010% or less. The B content is more preferably 0.0002% or more. The B content is more preferably 0.0050% or less. The B content is further preferably 0.0004% or more. The B content is further preferably 0.0030% or less.
- In addition to the composition described above, the hot rolled steel sheet may contain one or more of REM, Zr, As, Cu, Ni, Sn, Pb, Ta, W, Cr, Sb, Mg, Ca, Co, Se, Zn, and Cs so that their total content is 1.0% or less.
- The components other than those described above are Fe and incidental impurities.
- The reasons for limiting the microstructure in the hot rolled steel sheet are given below.
- The hot rolled steel sheet has a microstructure mainly composed of tempered bainite and tempered martensite having both high strength and excellent blanking workability. If the total area ratio of tempered bainite phase and tempered martensite phase is less than 70%, the hot rolled steel sheet cannot have desired high strength and blanking workability. Here, the ratio of each of tempered bainite phase and tempered martensite is not individually defined because tempered bainite and tempered martensite after annealing are microstructures not distinguishable from each other. This is a major factor that can reduce variations in mechanical properties after annealing in the case where the manufacturing conditions during hot rolling vary. The total area ratio of tempered bainite phase and tempered martensite phase is therefore 70% or more. The total area ratio of tempered bainite phase and tempered martensite phase is preferably 75% or more. The total area ratio of tempered bainite phase and tempered martensite phase is more preferably 80% or more. The total area ratio of tempered bainite phase and tempered martensite phase may be 100%.
- As mentioned above, the microstructure of the hot rolled steel sheet is mainly composed of tempered bainite and tempered martensite, with the balance other than tempered bainite and tempered martensite being, for example, Fe-based carbides, coarse pearlite, fine pearlite, degenerate pearlite, bainite, martensite, and retained austenite. Of these, particularly in the case where coarse pearlite, martensite, and retained austenite are present in the metallic microstructure, stretch flangeability decreases noticeably. The total area ratio of coarse pearlite phase, martensite phase, and retained austenite phase is therefore 10% or less. The total area ratio of coarse pearlite phase, martensite phase, and retained austenite phase is preferably 8% or less. The total area ratio of coarse pearlite phase, martensite phase, and retained austenite phase is more preferably 5% or less. The total area ratio of coarse pearlite phase, martensite phase, and retained austenite phase may be 0%.
- Here, coarse pearlite has a lamellar spacing of 0.2 µm or more, fine pearlite has a lamellar spacing of less than 0.2 µm, and degenerate pearlite is a phase in which pearlite lamellar is not clearly observable. The lamellar spacing can be measured by microstructure observation using a scanning electron microscope.
- The balance other than tempered bainite phase, tempered martensite phase, coarse pearlite phase, martensite phase, and retained austenite phase is, for example, ferrite phase, degenerate pearlite phase, and fine pearlite phase. A total area ratio of such balance of 30% or less is allowable.
- For strengthening by tempered bainite phase and tempered martensite phase, it is important that tempered bainite phase and tempered martensite phase have fine laths with an average width of 1.0 µm or less as their substructure.
FIG. 1 is a schematic diagram illustrating an example of a microstructure in which tempered bainite phase and tempered martensite phase have laths as their substructure and Fe-based carbides precipitate and MC-type carbides disperse and precipitate inside and at the boundaries of the laths. If the laths disappears as a result of recovery or the average width of the laths is more than 1.0 µm, predetermined high strength cannot be achieved. The average width of laths which tempered bainite phase and tempered martensite phase have as their substructure is therefore 1.0 µm or less. The average width of laths is preferably 0.8 µm or less. The average width of laths is more preferably 0.6 µm or less. No lower limit is placed on the average width of laths, yet the lower limit is typically about 0.1 µm. - Fe-based carbides precipitated inside and at the boundaries of laths as illustrated in
FIG. 1 serve as a void origin during blanking, thus contributing to improved blanking workability. This effect is particularly high with Fe-based carbides having an aspect ratio of 5 or less. By setting the proportion of such Fe-based carbides to 80% or more, excellent blanking workability can be achieved. The proportion of Fe-based carbides with an aspect ratio of 5 or less in Fe-based carbides precipitated inside and at the boundaries of laths is therefore 80% or more. The proportion is preferably 85% or more. No upper limit is placed on the proportion, yet the upper limit may be 100%. - Fe-based carbides are θ carbide (cementite), ε carbide, and the like. An alloying element may be dissolved in the carbides. The aspect ratio is the ratio of the major axis length and minor axis length of Fe-based carbides precipitated inside and at the boundaries of laths.
- MC-type carbides finely dispersed and precipitated inside and at the boundaries of laths as illustrated in
FIG. 1 inhibit lath coarsening by a pinning effect when annealing the steel sheet and also inhibit lath disappearance resulting from recovery, thus contributing to higher strength. If the average particle size of MC-type carbides is more than 20 nm, the number of particles of MC-type carbides contributing to pinning is insufficient and so the pinning effect is insufficient, causing a decrease in steel sheet strength. If the average particle size of MC-type carbides is 20 nm or less, a sufficient number of particles of MC-type carbides exhibit the pinning effect, to prevent a decrease in steel sheet strength. The average particle size of MC-type carbides dispersed and precipitated inside and at the boundaries of laths of tempered bainite phase and tempered martensite phase is therefore 20 nm or less. The average particle size is preferably 15 nm or less. No lower limit is placed on the average particle size, yet the lower limit is typically about 1 nm. The proportion of MC-type carbides with a particle size of more than 50 nm is preferably 10% or less. - It is also important that the hot rolled steel sheet has an average dislocation density in the following range.
- The variations of the hot rolled steel sheet caused by the variations of the hot rolling conditions are reduced by tempering the steel sheet having bainite and martensite microstructure. If the average dislocation density of the steel sheet after annealing is more than 5.0 × 1015 m-2, the tempering of the steel sheet is insufficient and the influence of the variations of the hot rolling conditions cannot be reduced sufficiently. In the case where tempering is sufficient, the average dislocation density is typically 1.0 × 1014 m-2 or more. The average dislocation density is therefore 1.0 × 1014 m-2 or more and 5.0 × 1015 m-2 or less. The average dislocation density is preferably 1.0 × 1014 m-2 or more. The average dislocation density is preferably 2.0 × 1015 m-2 or less.
- A method of manufacturing the hot rolled steel sheet according to the disclosure is described below.
- The method of manufacturing the hot rolled steel sheet includes: hot rolling a steel raw material having the chemical composition described above, whereby the steel raw material is heated to an austenite single phase region, subjected to rough rolling and finish rolling to obtain a steel sheet, and the steel sheet is cooled and coiled after the finish rolling; pickling the steel sheet after the hot rolling; and then continuous annealing the steel sheet, wherein in the hot rolling, a finisher delivery temperature is 850 °C or more and 1000 °C or less, an average cooling rate to 500 °C after the finish rolling is 30 °C/s or more, and a coiling temperature is 500 °C or less, and in the continuous annealing, a maximum heating temperature of the steel sheet is 700 °C or more and (A3 point + A1 point)/2 or less, a time during which a temperature of the steel sheet is 600 °C or more and 700 °C or less in heating the steel sheet to the maximum heating temperature is 20 s or more and 1000 s or less, a time during which the temperature of the steel sheet is more than 700 °C is 200 s or less, an average cooling rate to 530 °C when cooling the steel sheet from the maximum heating temperature is 8 °C/s or more and 25 °C/s or less, and a time of holding the steel sheet in a temperature range of 470 °C or more and 530 °C or less after the cooling stops is 10 s or more. The method may further include performing a coating or plating treatment on the steel sheet, after the continuous annealing.
- The method of obtaining the steel raw material by steelmaking is not limited, and any known steelmaking process such as a converter steelmaking process or an electric furnace steelmaking process may be used. After steelmaking, continuous casting is preferably performed to yield a slab (steel raw material) in terms of productivity and the like. The slab may be yielded by a known casting method such as ingot casting and blooming, thin slab continuous casting, or the like.
- The obtained steel raw material is subjected to hot rolling, in which the steel raw material is subjected to rough rolling and finish rolling. Before the rough rolling, the steel raw material is heated in the austenite single phase region. If the steel raw material before the rough rolling is not heated in the austenite single phase region, the remelting of Ti carbide and the like present in the steel raw material does not progress, and fine MC-type carbides do not precipitate during the annealing after the hot rolling. Accordingly, the steel raw material is heated to 1150 °C or more, before the rough rolling. No upper limit is placed on the heating temperature, yet an excessively high heating temperature leads to a considerable decrease in yield rate due to the oxidation of the slab surface, and so the heating temperature is typically 1350 °C or less. In the case where the temperature of the cast steel raw material (slab) is in the austenite single phase region when hot rolling the steel raw material, the steel raw material may be subjected to hot direct rolling without being heated or after being heated for a short time.
- The reasons for limiting the manufacturing conditions in the hot rolling are given below.
- If the finisher delivery temperature is low, ferrite transformation is promoted during the cooling after the rolling, causing a decrease in the bainite and martensite ratio of the hot rolled steel sheet after the hot rolling. This makes it impossible to obtain a predetermined tempered bainite and tempered martensite ratio after the annealing. Accordingly, the finisher delivery temperature needs to be 850 °C or more. The finisher delivery temperature is preferably 880 °C or more. If the finisher delivery temperature is more than 1000 °C, the surface characteristics of the steel sheet degrade. The finisher delivery temperature is therefore 1000 °C or less. The finisher delivery temperature is preferably 970 °C or less. Each of the temperatures such as the finisher delivery temperature and the coiling temperature mentioned here is the temperature of the steel sheet surface.
- When cooling the steel sheet after the finish rolling, if the cooling rate is insufficient, ferrite cannot be suppressed adequately, causing a decrease in the bainite and martensite ratio of the hot rolled steel sheet after the hot rolling. This makes it impossible to obtain a predetermined tempered bainite and tempered martensite ratio after the annealing. Accordingly, the cooling rate to 500 °C after the finish rolling needs to be 30 °C/s or more. The cooling rate is preferably 50 °C/s or more. No upper limit is placed on the cooling rate, yet the upper limit is typically about 300 °C/s.
- Appropriately adjusting the coiling temperature is important in controlling the steel sheet microstructure after the hot rolling. If the coiling temperature is more than 500 °C, the lath width of bainite increases. This makes it impossible to obtain a predetermined lath width of tempered bainite after the annealing. No lower limit is placed on the coiling temperature, yet an excessively low coiling temperature merely leads to higher cooling cost, and so the coiling temperature is preferably 0 °C or more. The coiling temperature is more preferably 200 °C or more.
- After the hot rolling, the hot rolled steel sheet is subjected to pickling and then to continuous annealing. The reasons for limiting the manufacturing conditions in the continuous annealing are given below.
- Appropriately adjusting the maximum heating temperature of the steel sheet in the continuous annealing is important in sufficiently reducing the influence of the variations of the manufacturing conditions in the hot rolling caused by the annealing and achieving desired high strength. If the maximum heating temperature of the steel sheet is less than 700 °C, the dislocation density in bainite and martensite is difficult to be controlled within an appropriate range, and so the influence of the variations of the manufacturing conditions in the hot rolling cannot be reduced sufficiently. Besides, if the heating temperature of the steel sheet is less than 700 °C, the aspect ratio of Fe-based carbides inside and between laths tends to be high, which makes it difficult to set the proportion of Fe-based carbides with an aspect ratio of 5 or less to be in a desired range. If the maximum heating temperature of the steel sheet is more than (A3 point + A1 point)/2, MC-type carbides coarsen noticeably, as a result of which lath coarsening in bainite and martensite cannot be inhibited adequately. Moreover, austenitizing is promoted, causing a decrease in the bainite and martensite ratio. This makes it impossible to obtain a desired tempered bainite and tempered martensite ratio. The maximum heating temperature of the steel sheet in the continuous annealing is therefore 700 °C or more and (A3 point + A1 point)/2 or less. The maximum heating temperature is preferably 700 °C or more. The maximum heating temperature is preferably {(A3 point + A1 point)/2} - 10 °C or less.
-
- Time during which the steel sheet temperature is 600 °C or more and 700 °C or less in heating the steel sheet to the maximum heating temperature: 20 s or more and 1000 s or less
- In heating the steel sheet to the maximum heating temperature, it is important to appropriately control heat hysteresis in imparting desired high strength and excellent blanking workability to the steel sheet. The pinning effect of MC-type carbides is used to inhibit lath coarsening, as mentioned above. To achieve the pinning effect, MC-type carbides need to be sufficiently dispersed in bainite and martensite before lath coarsening starts. According to our study, the precipitation of MC-type carbides begins to occur noticeably at 600 °C or more. Meanwhile, lath coarsening and disappearance are noticeable at more than 700 °C. Hence, lath coarsening and disappearance can be inhibited by holding the steel sheet temperature in the temperature range of 600 °C or more and 700 °C or less for a predetermined time so that MC-type carbides precipitate sufficiently. For sufficient precipitation of MC-type carbides, the holding time in this temperature range needs to be 20 s or more. If the holding time in the temperature range is insufficient, lath coarsening starts before MC-type carbides precipitate sufficiently, so that the pinning effect is insufficient and the laths coarsen. The holding time is preferably 35 s or more. The holding time is more preferably 50 s or more.
- If the holding time of the steel sheet temperature in the temperature range of 600 °C or more and 700 °C or less is more than 1000 s, Fe-based carbides precipitated inside and between laths dissolve again and move to prior austenite grain boundaries, packet grain boundaries, block grain boundaries, and the like. Thus, Fe-based carbides inside and between laths that effectively contribute to improved blanking workability no longer exist. Accordingly, to obtain a steel sheet having excellent blanking workability, the holding time of the steel sheet temperature in the temperature range of 600 °C or more and 700 °C or less needs to be 1000 s or less. The holding time is preferably 800 s or less. The holding time is more preferably 500 s or less. The steel sheet temperature mentioned here is the temperature of the steel sheet surface.
- When the steel sheet temperature is in the temperature range of more than 700 °C, lath coarsening is noticeable. The pinning effect of MC-type carbides finely dispersed and precipitated is used to prevent the movement of lath boundaries and inhibit lath coarsening, as mentioned above. The steel sheet strength is maintained in this way. If the holding time in this temperature range is excessively long, however, lath coarsening cannot be inhibited. Accordingly, the holding time of the steel sheet temperature in the temperature range of more than 700 °C is 200 s or less, in terms of preventing lath coarsening. The holding time is preferably 180 s or less. The holding time is more preferably 150 s or less. If the time during which the steel sheet temperature is more than 700 °C is less than 10 s, the ductility of the steel sheet decreases to some extent, and so the holding time is 10 s or more.
- When cooling the steel sheet after heating it to the maximum heating temperature in the continuous annealing, it is important to appropriately control the cooling rate in achieving excellent stretch flangeability.
Particularly in the case where the average cooling rate to 530 °C is less than 8 °C/s, pearlite transformation cannot be suppressed during the cooling, as a result of which coarse pearlite forms in a predetermined amount or more. This decreases stretch flangeability. If the average cooling rate is excessively high, holding the steel sheet in the temperature range of 470 °C or more and 530 °C or less for a predetermined time as mentioned below is difficult. The average cooling rate to 530 °C when cooling the steel sheet from the maximum heating temperature is therefore 25 °C/s or less. - In the continuous annealing, it is important to hold the steel sheet in the temperature range of 470 °C or more and 530 °C or less for a predetermined time after the aforementioned controlled cooling, in achieving excellent stretch flangeability. If the holding temperature after the cooling stops is more than 530 °C, coarse pearlite forms, causing a decrease in stretch flangeability. If the holding temperature after the cooling stops is less than 470 °C, the transformation from austenite to bainite delays. As a result, C concentrates in the non-transformed austenite region to stabilize austenite, hampering the completion of the transformation. In the subsequent cooling, non-transformed austenite transforms to martensite or remains in the steel sheet microstructure as retained austenite, so that stretch flangeability decreases. In the case where the steel sheet is held in the temperature range of 470 °C or more and 530 °C or less for 10 s or more, the transformation of most austenite to bainite completes, with it being possible to reduce the proportion of martensite which forms during the subsequent cooling to a predetermined range. Accordingly, the holding time in the temperature range of 470 °C or more and 530 °C or less after the controlled cooling stops is 10 s or more. The holding time is preferably 20 s or more. The holding time is more preferably 30 s or more. No upper limit is placed on the holding time, yet the holding time is typically 300 s or less.
- Holding the steel sheet in the temperature range of 470 °C or more and 530 °C or less completes the control of the steel sheet microstructure. The subsequent cooling conditions are not limited, and the steel sheet may be cooled to room temperature by any cooling method.
- Even in the case of reheating the steel sheet to 700 °C or less after holding the steel sheet in the temperature range of 470 °C or more and 530 °C or less, desired steel sheet microstructure can still be obtained as long as the total holding time in the temperature range of 600 °C or more and 700 °C or less is 1000 s or less.
- For example, after holding the steel sheet in the temperature range of 470 °C or more and 530 °C or less, the steel sheet may be immersed in a zinc pot to yield a hot-dip galvanized steel sheet. The steel sheet may then be further heated to yield a galvannealed steel sheet. The hot dip coating is not limited to zinc, and may be a coating of aluminum, an aluminum alloy, or the like.
- After the continuous annealing, the steel sheet may be subjected to temper rolling either continuously in the annealing line or using another line according to a conventional method.
- The hot rolled steel sheet manufactured as described above may be electrogalvanized or hot-dip galvanized. The hot rolled steel sheet according to the disclosure is suitable not only as a steel sheet for automotive suspension parts but also for press forming typically performed at ordinary temperature, and has excellent heat resistance. Hence, the hot rolled steel sheet manufactured as described above is also suitable as a blank sheet for a warm forming process of heating a steel sheet to 400 °C to 700 °C before pressing and then immediately press forming the steel sheet.
- Molten steels having the compositions listed in Table 1 were each obtained by steelmaking and subjected to continuous casting by a typically known technique, to yield a slab (steel raw material) with a thickness of 300 mm. The slab was heated to the temperature in Table 2, rough rolled, and finish rolled at the finisher delivery temperature in Table 2. After completing the finish rolling, the steel sheet was cooled at the average cooling rate in Table 2, and coiled at the coiling temperature in Table 2, to obtain a hot rolled steel sheet with a sheet thickness of 3.2 mm. The hot rolled steel sheet was then pickled by a typically known technique, and annealed in a continuous annealing line under the conditions in Table 2. Some of the steel sheets were subjected to hot-dip galvanizing treatment and optionally further subjected to alloying treatment in the continuous annealing line, thus yielding hot-dip galvanized steel sheets and galvannealed steel sheets.
Table 1 Steel No. Chemical composition (mass%) Remarks C Si Mn P S Al N Ti V Nb Mo B Others 1 0.024 0.06 0.7 0.025 0.002 0.04 0.0032 0.095 - - - - - Comparative steel 2 0.060 0.03 0.6 0.027 0.002 0.04 0.0057 0.090 - - - - - Conforming steel 3 0.140 0.05 0.7 0.026 0.003 0.03 0.0029 0.056 - - - - - Conforming steel 4 0.081 0.31 0.4 0.014 0.002 0.05 0.0035 0.096 - - - - - Comparative steel 5 0.128 0.17 1.2 0.020 0.002 0.04 0.0064 0.089 - - - - - Conforming steel 6 0.145 0.29 1.8 0.015 0.002 0.03 0.0037 0.082 - - - - - Conforming steel 7 0.177 0.07 2.5 0.025 0.002 0.03 0.0064 0.107 - - - - - Comparative steel 8 0.099 0.15 1.1 0.021 0.001 0.05 0.0027 0.024 - - - - - Comparative steel 9 0.147 0.30 1.6 0.014 0.003 0.03 0.0060 0.062 - - - - - Conforming steel 10 0.161 0.23 1.4 0.018 0.001 0.03 0.0047 0.113 - - - - - Conforming steel 11 0.053 0.30 1.6 0.015 0.002 0.06 0.0029 0.195 - - - - - Comparative steel 12 0.114 0.16 1.1 0.021 0.003 0.04 0.0056 0.048 - - - - - Conforming steel 13 0.163 0.10 0.9 0.024 0.003 0.03 0.0030 0.050 - - - - - Conforming steel 14 0.183 0.11 0.9 0.023 0.003 0.02 0.0031 0.045 - - - - - Conforming steel 15 0.049 0.19 1.2 0.019 0.002 0.06 0.0049 0.097 - - - - - Conforming steel 16 0.153 0.25 1.4 0.017 0.001 0.03 0.0051 0.134 - - - - - Conforming steel 17 0.163 0.19 1.2 0.019 0.003 0.03 0.0035 0.060 - - - - - Conforming steel 18 0.111 0.16 1.1 0.021 0.002 0.04 0.0037 0.072 - - - - - Conforming steel 19 0.056 0.15 1.1 0.021 0.002 0.06 0.0032 0.089 - - - - - Conforming steel 20 0.112 0.22 1.3 0.018 0.001 0.04 0.0037 0.123 - - - - - Conforming steel 21 0.128 0.22 1.3 0.018 0.003 0.04 0.0037 0.057 - - - - - Conforming steel 22 0.120 0.17 1.1 0.020 0.002 0.04 0.0045 0.108 - - - - - Conforming steel 23 0.129 0.03 1.5 0.011 0.002 0.04 0.0037 0.065 - - - 0.0015 - Conforming steel 24 0.144 0.24 1.4 0.017 0.002 0.03 0.0054 0.109 0.092 - - - As: 0.003 Conforming steel 25 0.173 0.35 1.8 0.012 0.001 0.03 0.0051 0.113 - 0.043 - - Ca: 0.004, Sn: 0.002 Conforming steel 26 0.048 0.34 1.8 0.012 0.001 0.06 0.0040 0.130 - - 0.15 - Se: 0.005, Cr.0.23 Conforming steel 27 0.174 0.37 1.9 0.011 0.001 0.03 0.0046 0.125 - - - 0.0019 Sb: 0.004, Cu: 0.09, Ni: 0.18 Conforming steel 28 0.139 0.32 1.7 0.014 0.002 0.04 0.0057 0.074 - - - 0.0013 Co: 0.028, Cs:0.004 Conformity steel 29 0.102 0.09 0.8 0.024 0.002 0.04 0.0055 0.099 - - - 0.0018 Mg: 0.006, Ta: 0.03 Conforming steel 30 0.090 0.26 1.5 0.017 0.002 0.05 0.0050 0.082 - - - 0.0017 Pb: 0.004, W: 0.12 Conforming steel 31 0.169 0.13 1.0 0.022 0.002 0.03 0.0044 0.079 0.046 - 0.10 - Zr: 0.04 Conforming steel 32 0.109 0.33 1.7 0.013 0.003 0.04 0.0056 0.065 - - - - Zn: 0.0012 Conforming steel 33 0.189 0.37 1.9 0.011 0.002 0.02 0.0030 0.075 - - - - REM: 0.06 Conforming steel Table 2 Steel sheet No Steel No. Hot rolling conditions Continious annealing conditions Conting or Plating treatment Albying treatment Remarks Slab heating temperature (°C) Finishes delivery temperature (°C) Average cooling rate*1 (°C/s) Coiling temperature (°C) Maximum heating temperature A1 *2 A3 *3 (A3+A1)/2 Holding time 1*4 Holding time 2*5 Average cooling rate *6 Holding time 3*7 (°C) (°C) (°C) (°C) (s) (s) (°C/s) (s) 1 1 1220 920 63 380 720 730 927 829 120 20 12 110 110 Comparative Example 2 2 1220 910 81 390 800 731 910 820 130 70 12 110 Example 3 3 1220 860 86 460 710 732 867 800 190 20 15 110 Performed Example 4 4 1220 950 46 390 830 736 921 829 150 100 13 80 Comparative Example 5 5 1220 890 64 410 730 725 874 800 170 30 14 60 Perfomed Performed Example 6 6 1220 950 78 360 790 721 860 790 210 70 16 110 Example 7 1 1220 950 68 460 760 708 822 765 40 50 9 70 Comparative Example 8 8 1220 850 47 340 710 730 881 805 110 20 12 90 Comparative Example 9 9 1220 920 52 460 780 724 960 792 170 60 14 50 Example 10 10 1200 900 83 330 750 724 862 793 190 40 15 70 Performed Performed Example 11 11 1200 860 52 360 710 715 923 819 60 20 9 50 Compartive Example 12 12 1200 900 60 470 780 728 876 802 130 60 13 80 Perfomed Comparative Example 13 13 1200 830 60 470 731 854 792 190 20 15 100 Comparative Example 14 14 1200 870 17 480 710 731 844 787 220 20 16 90 15 15 1220 900 80 560 770 724 914 819 50 50 9 80 Comparative Example 16 16 1220 900 76 300 640 722 868 795 180 0 14 60 Comparative Example 17 17 1220 890 59 450 850 728 854 791 190 80 15 80 Comparative Example 18 18 1220 890 76 430 730 727 881 804 15 30 12 80 Comparative Example 19 19 1220 880 70 390 720 725 910 817 1150 20 10 90 Comparative Example 20 20 1220 890 49 320 730 722 887 804 130 230 12 70 Comparator Example 21 21 1220 890 84 460 770 726 870 798 150 20 4 70 Comparative Example 22 22 1220 900 69 350 760 725 881 803 140 30 13 5 Comparative Example 23 23 1180 920 58 450 740 719 861 790 110 50 13 70 Performed Performed Example 24 24 1180 900 58 350 770 720 880 800 170 50 14 70 Performed Performed Example 25 25 1220 900 45 340 760 731 853 792 210 40 15 40 Performed Performed Example 26 26 1220 890 49 310 750 721 922 821 50 50 9 40 Performed Performed Example 27 27 1220 900 85 320 750 718 861 789 210 50 15 40 Performed Exemple 28 28 1220 910 57 420 780 722 869 796 160 40 14 50 Performed Example 29 29 1220 900 79 370 780 725 896 811 120 40 12 100 Performed Example 30 30 1220 900 76 410 770 722 896 809 100 60 11 60 Example 31 31 1220 890 78 410 750 729 865 797 450 60 15 90 Example 32 32 1220 910 60 440 780 723 878 801 190 50 12 50 Example 33 33 1220 870 75 420 710 722 841 782 540 40 16 40 Example *1 average cooling rate until steel sheet temperature reaches 500°C after finish rolling
*2 A1 point = 751-26.6×[%C]+17.6×[%Si]-11.6×[%Mn]+22.5×[%Mo]+233×[%Nb]-39.7×[%V]-57×[%Ti]-895×[%B]-169×[%Al] ([%X] is content of X elemert n steel (mass%))
*3 A3 point = 937-476.55×[%C]+56×[%Si]-19.7×[%Mn]+38.1×[%Mo]+124.8×[%V]+136.3×[%Ti]-19×[%Nb]+3315×[%B] ([%X] is content of X element in steel (mass%))
*4 holding time of steel shed temperature in temperature range of 600°C or more and 700°C or less
*5 holing time of steel sheet temperature in temperature range of more than 700°C
*6 average cooling rate fom maximum heating temperature to 530°C
*7 holding time in temperature range ef 470°C or more and 530°C or less after cooling stops - A test piece was collected from each obtained hot rolled steel sheet, and subjected to microstructure observation, average dislocation density measurement, a tensile test, a hole expansion test, a blanking test, and manufacturing stability evaluation. The evaluation results are listed in Table 3. The test methods are as follows.
- A test piece was collected from each obtained hot rolled steel sheet, and polished in a cross-section (L cross-section) parallel to the rolling direction of the test piece and etched by nital. A micrograph taken with a scanning electron microscope (1000, 3000, 5000 magnifications) was used to determine the total area ratio of tempered bainite phase and tempered martensite phase, the area ratio of coarse pearlite phase, the total area ratio of martensite phase and retained austenite phase (MA), and the area ratio of phase other than these, through the use of an image analyzer. It is difficult to distinguish martensite phase and retained austenite phase from each other with a scanning electron micrograph. In this example, however, the total area ratio of coarse pearlite phase, martensite phase, and retained austenite phase is important, and accordingly the total area ratio of martensite phase and retained austenite phase (MA) was determined without distinguishing martensite phase and retained austenite phase from each other.
- Moreover, a thin film made from each hot rolled steel sheet was observed using a transmission electron microscope (TEM), to measure the lath width in tempered bainite and tempered martensite and determine the proportion of Fe-based carbides with an aspect ratio of 5 or less in Fe-based carbides precipitated inside and at the boundaries of laths and the average particle size of MC-type carbides precipitated inside and at the boundaries of laths.
- The lath width in tempered bainite and tempered martensite was measured as follows. In a transmission electron micrograph of 120 mm × 80 mm in size taken for 10 observation fields at 30000 magnifications, five straight lines orthogonal to the major axes of three or more consecutively aligned laths were drawn at intervals of 10 mm, the length of each line segment where the corresponding straight line intersects with the lath boundaries was measured, and the average length of the line segments was set as the average lath width.
- The proportion of Fe-based carbides with an aspect ratio of 5 or less in Fe-based carbides precipitated inside and at the boundaries of laths was determined as follows. In a micrograph taken at 165000 magnifications, the major axis length and the minor axis length were measured for at least 100 particles of Fe-based carbides precipitated inside and at the boundaries of laths for 5 observation fields in total, to calculate the aspect ratio. The proportion of Fe-based carbides with an aspect ratio of 5 or less was thus determined.
- The average particle size of MC-type carbides was determined as follows. In a micrograph taken at 300000 magnifications, the diameter was measured for at least 100 particles of MC-type carbides such as TiC for 5 observation fields in total, and an arithmetic average (average particle size ddef) was calculated. The lower limit of the measured particle size was 2 nm.
- A test piece was collected from each obtained hot rolled steel sheet, and the dislocation density of a 1/4 portion in sheet thickness was measured. Assuming that the dislocation density of a 1/4 portion in sheet thickness represents the average dislocation density of the steel sheet, the measurement was set as average dislocation density. The collected test piece was subjected to mechanical grinding and also polishing with oxalic acid for 0.1 mm, to adjust the sample so that the 1/4 portion in sheet thickness was exposed to the surface. Polishing with oxalic acid was intended to remove the layer worked by grinding.
- For the sample adjusted in this way, the strain of the steel sheet was measured by an X-ray diffractometer. With an X-ray diffractometer, the diffraction intensity of (110) plane, (211) plane, and (220) plane of α-iron in the 1/4 portion in sheet thickness was measured using CoKα rays. The half-value breadth of the peak value of the reflection intensity of each crystal plane was calculated from the obtained measurement chart, and the local strain ε' applied to the steel sheet was determined according to the following Expressions (1) and (2).
- where βm is the half-value breadth of the peak of the sample subjected to dislocation density measurement, and β0 is the half-value breadth of the peak of a strain-free sample.
-
- A JIS No. 5 tensile test piece (JIS Z 2001) was collected from each obtained hot rolled steel sheet so that the direction (C direction) orthogonal to the rolling direction was the tensile direction, and subjected to a tensile test in conformity with JIS Z 2241 to measure yield strength (YS), tensile strength (TS), and elongation (EI).
- A test piece (size: 100 mm × 100 mm) was collected from each obtained hot rolled steel sheet, and blanked with a hole of 10 mmφ in initial diameter d0 (clearance: 12.5% of the test piece sheet thickness). A hole expansion test was conducted using the test piece. In detail, a conical punch with a vertex angle of 60° was inserted into the hole of 10 mmφ in initial diameter d0 from the punch side at the time of blanking, to expand the hole. The diameter d (mm) of the hole when a crack ran through the steel sheet (test piece) was measured, and the hole expansion ratio λ (%) was calculated according to the following expression.
- The stretch flangeability was evaluated as favorable in the case where tensile strength (TS) × {hole expansion ratio (λ)}0.5 was 6200·MPa%0.5 or more.
- A test piece (size: 30 mm × 30 mm) was collected from each obtained hot rolled steel sheet, and blanked with a hole of 10 mmφ in diameter d0 (clearance: 20%, 30% of the test piece sheet thickness). After the blanking, the fracture state of the punched end surface was observed by a microscope (50 magnifications) on the whole circumference of the punch hole, to observe whether or not any crack, chip, or brittle fracture occurred. The blanking workability was evaluated as "pass" if there was no crack, chip, or brittle fracture, and "fail" otherwise.
- As can be seen from Table 3, in all Examples, a hot rolled steel sheet having high strength such as a tensile strength (TS) of 780 MPa or more and excellent stretch flangeability and blanking workability was obtained.
- To evaluate the variations of the mechanical properties of each steel sheet, 100 JIS No. 5 tensile test pieces (JIS Z 2001) were optionally collected from the whole length and whole width of the hot rolled steel sheets of Examples so that the orthogonal direction (C direction) was the tensile direction. A tensile test was conducted in conformity with JIS Z 2241 to measure the tensile strength (TS), and their standard deviation σ was calculated. In all Examples, the standard deviation of the tensile strength (TS) was 10 MPa or less.
- Thus, in all Examples, the mechanical properties of the steel sheet such as tensile strength (TS) had little variations, exhibiting excellent manufacturing stability.
Claims (4)
- A hot rolled steel sheet comprising:a composition containing, in mass%,C: 0.03% or more and 0.20% or less,Si: 0.4% or less,Mn: 0.5% or more and 2.0% or less,P: 0.03% or less,S: 0.03% or less,Al: 0.1% or less,N: 0.01% or less, andTi: 0.03% or more and 0.15% or less,optionally one or more ofV: 0.01% or more and 0.3% or less,Nb: 0.01% or more and 0.1% or less,Mo: 0.01% or more and 0.3% or less,B: 0.0002% or more and 0.010% or less,REM, Zr, As, Cu, Ni, Sn, Pb, Ta, W, Cr, Sb, Mg, Ca, Co, Se, Zn, and Cs: 1.0% or less in total,with a balance being Fe and incidental impurities;a microstructure in which a total area ratio of a tempered bainite phase and a tempered martensite phase is 70% or more, a total area ratio of a coarse pearlite phase, a martensite phase, and a retained austenite phase is 10% or less, the tempered bainite phase and the tempered martensite phase have laths with an average width of 1.0 µm or less as a substructure, a proportion of Fe-based carbides with an aspect ratio of 5 or less in Fe-based carbides precipitated inside and at boundaries of the laths is 80% or more, and MC-type carbides with an average particle size of 20 nm or less are dispersed and precipitated inside and at the boundaries of the laths; andan average dislocation density of 1.0 × 1014 m-2 or more and 5.0 × 1015 m-2 or less.
- The hot rolled steel sheet according to claim 1, comprising a coated or plated layer on a surface thereof.
- A method of manufacturing a hot rolled steel sheet, comprising:hot rolling a steel raw material having the composition according to claim 1, whereby the steel raw material is heated to an austenite single phase region at a temperature of 1150 °C or more and subjected to rough rolling and finish rolling to obtain a steel sheet, and the steel sheet is cooled and coiled after the finish rolling;pickling the steel sheet after the hot rolling; andthen continuous annealing the steel sheet,wherein in the hot rolling, a finisher delivery temperature is 850 °C or more and 1000 °C or less, an average cooling rate to 500 °C after the finish rolling is 30 °C/s or more, and a coiling temperature is 500 °C or less, andin the continuous annealing, a maximum heating temperature of the steel sheet is 700 °C or more and (A3 point + A1 point)/2 or less, a time during which a temperature of the steel sheet is 600 °C or more and 700 °C or less in heating the steel sheet to the maximum heating temperature is 20 s or more and 1000 s or less, a time during which the temperature of the steel sheet is more than 700 °C is 10 s or more and 200 s or less, an average cooling rate to 530 °C when cooling the steel sheet from the maximum heating temperature is 8 °C/s or more and 25 °C/s or less, and a time of holding the steel sheet in a temperature range of 470 °C or more and 530 °C or less after the cooling stops is 10 s or more.
- The method of manufacturing a hot rolled steel sheet according to claim 3, further comprising
performing a coating or plating treatment on the steel sheet, after the continuous annealing.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2015075329 | 2015-04-01 | ||
PCT/JP2016/001834 WO2016157896A1 (en) | 2015-04-01 | 2016-03-30 | Hot-rolled steel sheet and method for producing same |
Publications (3)
Publication Number | Publication Date |
---|---|
EP3279353A1 EP3279353A1 (en) | 2018-02-07 |
EP3279353A4 EP3279353A4 (en) | 2018-02-07 |
EP3279353B1 true EP3279353B1 (en) | 2019-03-27 |
Family
ID=57004085
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP16771783.4A Active EP3279353B1 (en) | 2015-04-01 | 2016-03-30 | Hot-rolled steel sheet and method for producing same |
Country Status (7)
Country | Link |
---|---|
US (1) | US20180119240A1 (en) |
EP (1) | EP3279353B1 (en) |
JP (1) | JP6075517B1 (en) |
KR (1) | KR101989262B1 (en) |
CN (1) | CN107429362B (en) |
MX (1) | MX2017012493A (en) |
WO (1) | WO2016157896A1 (en) |
Families Citing this family (20)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP3473741B1 (en) * | 2016-08-30 | 2020-05-13 | JFE Steel Corporation | Thin steel sheet and process for producing same |
KR101867701B1 (en) * | 2016-11-11 | 2018-06-15 | 주식회사 포스코 | Pressure vessel steel plate with excellent hydrogen induced cracking resistance and manufacturing method thereof |
JP6424908B2 (en) * | 2017-02-06 | 2018-11-21 | Jfeスチール株式会社 | Hot-dip galvanized steel sheet and method of manufacturing the same |
JP6816550B2 (en) * | 2017-02-17 | 2021-01-20 | 日本製鉄株式会社 | Black surface-coated high-strength molten Zn-Al-Mg-based plated steel sheet with excellent bending workability and its manufacturing method |
KR102043511B1 (en) * | 2017-12-12 | 2019-11-12 | 주식회사 포스코 | Quenched high carbon steel sheet and method for manufacturing the same |
KR102031445B1 (en) * | 2017-12-22 | 2019-10-11 | 주식회사 포스코 | High strength steel sheet having excellent impact resistance property and method for manufacturing the same |
EP3786310A4 (en) * | 2018-04-23 | 2022-01-19 | Nippon Steel Corporation | Steel member and method for producing same |
KR102495085B1 (en) | 2018-07-31 | 2023-02-06 | 제이에프이 스틸 가부시키가이샤 | Thin steel sheet and its manufacturing method |
KR102075642B1 (en) * | 2018-08-06 | 2020-02-10 | 주식회사 포스코 | High strenghth hot-rolled plated steel sheet having excellent hole flangeability, and method of manufacturing the same |
US20220056543A1 (en) * | 2018-09-20 | 2022-02-24 | Arcelormittal | Hot rolled steel sheet with high hole expansion ratio and manufacturing process thereof |
JP6773252B2 (en) * | 2018-10-19 | 2020-10-21 | 日本製鉄株式会社 | Hot-rolled steel sheet |
EP3653736B1 (en) * | 2018-11-14 | 2020-12-30 | SSAB Technology AB | Hot-rolled steel strip and manufacturing method |
JP7168088B2 (en) * | 2019-07-10 | 2022-11-09 | 日本製鉄株式会社 | high strength steel plate |
JP7147960B2 (en) * | 2019-11-27 | 2022-10-05 | Jfeスチール株式会社 | Steel plate and its manufacturing method |
US20230002848A1 (en) * | 2019-12-23 | 2023-01-05 | Nippon Steel Corporation | Hot-rolled steel sheet |
JP7287334B2 (en) * | 2020-04-22 | 2023-06-06 | Jfeスチール株式会社 | High-strength steel plate and its manufacturing method |
CN112375891A (en) * | 2020-10-20 | 2021-02-19 | 包头钢铁(集团)有限责任公司 | Online tempering process for eliminating bainite steel rail tensile fracture brittleness platform |
MX2024006055A (en) * | 2021-11-26 | 2024-06-04 | Nippon Steel Corp | Zinc-plated steel sheet. |
KR20240099378A (en) * | 2022-01-07 | 2024-06-28 | 닛폰세이테츠 가부시키가이샤 | hot rolled steel plate |
CN115354237B (en) * | 2022-08-29 | 2023-11-14 | 东北大学 | Hot-rolled ultrahigh-strength steel plate with tensile strength of 1000MPa and preparation method thereof |
Family Cites Families (26)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP3244986B2 (en) * | 1995-02-06 | 2002-01-07 | 新日本製鐵株式会社 | Weldable high strength steel with excellent low temperature toughness |
US7090731B2 (en) * | 2001-01-31 | 2006-08-15 | Kabushiki Kaisha Kobe Seiko Sho (Kobe Steel, Ltd.) | High strength steel sheet having excellent formability and method for production thereof |
JP3698058B2 (en) * | 2001-02-13 | 2005-09-21 | 住友金属工業株式会社 | High Cr ferritic heat resistant steel |
JP4156889B2 (en) * | 2001-10-03 | 2008-09-24 | 株式会社神戸製鋼所 | Composite steel sheet with excellent stretch flangeability and method for producing the same |
FR2830260B1 (en) * | 2001-10-03 | 2007-02-23 | Kobe Steel Ltd | DOUBLE-PHASE STEEL SHEET WITH EXCELLENT EDGE FORMABILITY BY STRETCHING AND METHOD OF MANUFACTURING THE SAME |
JP4956998B2 (en) * | 2005-05-30 | 2012-06-20 | Jfeスチール株式会社 | High-strength hot-dip galvanized steel sheet with excellent formability and method for producing the same |
JP5326344B2 (en) * | 2007-04-27 | 2013-10-30 | 新日鐵住金株式会社 | Heat-resistant structure with excellent creep characteristics in heat-affected zone |
MX2011012371A (en) * | 2009-05-27 | 2011-12-08 | Nippon Steel Corp | High-strength steel sheet, hot-dipped steel sheet, and alloy hot-dipped steel sheet that have excellent fatigue, elongation, and collision characteristics, and manufacturing method for said steel sheets. |
JP5728836B2 (en) * | 2009-06-24 | 2015-06-03 | Jfeスチール株式会社 | Manufacturing method of high strength seamless steel pipe for oil wells with excellent resistance to sulfide stress cracking |
JP5765080B2 (en) * | 2010-06-25 | 2015-08-19 | Jfeスチール株式会社 | High-strength hot-rolled steel sheet excellent in stretch flangeability and manufacturing method thereof |
JP5609786B2 (en) | 2010-06-25 | 2014-10-22 | Jfeスチール株式会社 | High-tensile hot-rolled steel sheet excellent in workability and manufacturing method thereof |
JP5724267B2 (en) * | 2010-09-17 | 2015-05-27 | Jfeスチール株式会社 | High-strength hot-rolled steel sheet excellent in punching workability and manufacturing method thereof |
JP5126326B2 (en) * | 2010-09-17 | 2013-01-23 | Jfeスチール株式会社 | High strength hot-rolled steel sheet with excellent fatigue resistance and method for producing the same |
MX361834B (en) * | 2010-10-22 | 2018-12-18 | Nippon Steel & Sumitomo Metal Corp | Steel sheet and steel sheet production process. |
JP5780086B2 (en) * | 2011-09-27 | 2015-09-16 | Jfeスチール株式会社 | High strength steel plate and manufacturing method thereof |
TWI507538B (en) * | 2011-09-30 | 2015-11-11 | Nippon Steel & Sumitomo Metal Corp | With excellent burn the attachment strength of the hardenable galvannealed steel sheet, a high strength galvannealed steel sheet and manufacturing method, etc. |
EP2765212B1 (en) * | 2011-10-04 | 2017-05-17 | JFE Steel Corporation | High-strength steel sheet and method for manufacturing same |
JP5541263B2 (en) * | 2011-11-04 | 2014-07-09 | Jfeスチール株式会社 | High-strength hot-rolled steel sheet excellent in workability and manufacturing method thereof |
KR20140110996A (en) * | 2012-01-06 | 2014-09-17 | 제이에프이 스틸 가부시키가이샤 | High strength hot-rolled steel sheet and method for producing same |
JP5429331B2 (en) * | 2012-07-13 | 2014-02-26 | Jfeスチール株式会社 | High-strength cold-rolled steel sheet with excellent manufacturing stability and manufacturing method thereof |
CA2880946C (en) * | 2012-08-15 | 2018-06-12 | Nippon Steel & Sumitomo Metal Corporation | Steel sheet for hot stamping, method of manufacturing the same, and hot stamped steel sheet member |
JP5637225B2 (en) * | 2013-01-31 | 2014-12-10 | Jfeスチール株式会社 | High-strength hot-rolled steel sheet excellent in burring workability and manufacturing method thereof |
BR112015023632B1 (en) * | 2013-04-04 | 2020-04-28 | Jfe Steel Corp | hot rolled steel sheet and method for producing it |
JP5641087B2 (en) | 2013-04-15 | 2014-12-17 | Jfeスチール株式会社 | High-strength hot-rolled steel sheet excellent in mass production punchability and manufacturing method thereof |
CN105143485B (en) * | 2013-04-15 | 2017-08-15 | 杰富意钢铁株式会社 | High tensile hot rolled steel sheet and its manufacture method |
JP6136547B2 (en) * | 2013-05-07 | 2017-05-31 | 新日鐵住金株式会社 | High yield ratio high strength hot-rolled steel sheet and method for producing the same |
-
2016
- 2016-03-30 KR KR1020177029834A patent/KR101989262B1/en active IP Right Grant
- 2016-03-30 WO PCT/JP2016/001834 patent/WO2016157896A1/en active Application Filing
- 2016-03-30 MX MX2017012493A patent/MX2017012493A/en unknown
- 2016-03-30 EP EP16771783.4A patent/EP3279353B1/en active Active
- 2016-03-30 CN CN201680020526.3A patent/CN107429362B/en active Active
- 2016-03-30 US US15/561,436 patent/US20180119240A1/en not_active Abandoned
- 2016-03-30 JP JP2016549181A patent/JP6075517B1/en active Active
Non-Patent Citations (1)
Title |
---|
None * |
Also Published As
Publication number | Publication date |
---|---|
EP3279353A1 (en) | 2018-02-07 |
WO2016157896A1 (en) | 2016-10-06 |
KR101989262B1 (en) | 2019-06-13 |
JP6075517B1 (en) | 2017-02-08 |
KR20170128555A (en) | 2017-11-22 |
CN107429362B (en) | 2020-06-23 |
MX2017012493A (en) | 2018-01-18 |
US20180119240A1 (en) | 2018-05-03 |
EP3279353A4 (en) | 2018-02-07 |
JPWO2016157896A1 (en) | 2017-04-27 |
CN107429362A (en) | 2017-12-01 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP3279353B1 (en) | Hot-rolled steel sheet and method for producing same | |
EP3564400B1 (en) | High-strength galvanized steel sheet and method for manufacturing same | |
EP3444372B1 (en) | High strength steel sheet and manufacturing method therefor | |
EP3128023B1 (en) | High-yield-ratio high-strength cold rolled steel sheet and production method therefor | |
EP3187601B1 (en) | High-strength steel sheet and method for manufacturing same | |
EP3178949B1 (en) | High-strength steel sheet and method for manufacturing same | |
EP3178955B1 (en) | High-strength steel sheet and production method for same, and production method for high-strength galvanized steel sheet | |
EP3178957B1 (en) | High-strength steel sheet and production method for same, and production method for high-strength galvanized steel sheet | |
EP3272892B1 (en) | High-strength cold-rolled steel sheet and method for manufacturing same | |
EP3214199B1 (en) | High-strength steel sheet, high-strength hot-dip galvanized steel sheet, high-strength hot-dip aluminum-coated steel sheet, and high-strength electrogalvanized steel sheet, and methods for manufacturing same | |
EP2799578B1 (en) | High-strength hot-rolled steel sheet and manufacturing method therefor | |
EP3875615B1 (en) | Steel sheet, member, and methods for producing them | |
CN109072371B (en) | High-strength steel sheet for warm working and method for producing same | |
EP3415655B1 (en) | High-strength steel sheet and method for manufacturing same | |
EP3438311B1 (en) | Steel sheet, coated steel sheet, method for producing hot-rolled steel sheet, method for producing cold-rolled full hard steel sheet, method for producing heat-treated steel sheet, method for producing steel sheet, and method for producing coated steel sheet | |
EP2765211B1 (en) | High-tensile-strength hot-rolled steel sheet and method for producing same | |
EP3447159B1 (en) | Steel plate, plated steel plate, and production method therefor | |
EP3263727B1 (en) | High-strength cold-rolled steel plate and method for producing same | |
EP3255163B1 (en) | High-strength steel sheet and production method therefor | |
EP3757242A1 (en) | High-strength steel sheet and manufacturing method therefor | |
EP3705592A1 (en) | High-strength cold-rolled steel sheet, high-strength plated steel sheet, and production methods therefor | |
EP3875616B1 (en) | Steel sheet, member, and methods for producing them | |
US11117348B2 (en) | High-strength hot-rolled coated steel sheet | |
EP3543365B1 (en) | High-strength steel sheet and method for producing same | |
EP3916115A1 (en) | High-strength steel sheet and method for manufacturing same |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: THE INTERNATIONAL PUBLICATION HAS BEEN MADE |
|
PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: REQUEST FOR EXAMINATION WAS MADE |
|
17P | Request for examination filed |
Effective date: 20171016 |
|
A4 | Supplementary search report drawn up and despatched |
Effective date: 20180104 |
|
AK | Designated contracting states |
Kind code of ref document: A1 Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR |
|
AX | Request for extension of the european patent |
Extension state: BA ME |
|
DAV | Request for validation of the european patent (deleted) | ||
DAX | Request for extension of the european patent (deleted) | ||
GRAP | Despatch of communication of intention to grant a patent |
Free format text: ORIGINAL CODE: EPIDOSNIGR1 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: GRANT OF PATENT IS INTENDED |
|
INTG | Intention to grant announced |
Effective date: 20181026 |
|
GRAS | Grant fee paid |
Free format text: ORIGINAL CODE: EPIDOSNIGR3 |
|
GRAA | (expected) grant |
Free format text: ORIGINAL CODE: 0009210 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: THE PATENT HAS BEEN GRANTED |
|
AK | Designated contracting states |
Kind code of ref document: B1 Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR |
|
REG | Reference to a national code |
Ref country code: GB Ref legal event code: FG4D |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: EP |
|
REG | Reference to a national code |
Ref country code: AT Ref legal event code: REF Ref document number: 1113177 Country of ref document: AT Kind code of ref document: T Effective date: 20190415 |
|
REG | Reference to a national code |
Ref country code: IE Ref legal event code: FG4D |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R096 Ref document number: 602016011663 Country of ref document: DE |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: SE Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20190327 Ref country code: FI Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20190327 Ref country code: NO Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20190627 Ref country code: LT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20190327 |
|
REG | Reference to a national code |
Ref country code: NL Ref legal event code: MP Effective date: 20190327 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: GR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20190628 Ref country code: NL Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20190327 Ref country code: RS Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20190327 Ref country code: HR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20190327 Ref country code: LV Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20190327 Ref country code: BG Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20190627 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: FR Payment date: 20190427 Year of fee payment: 4 |
|
REG | Reference to a national code |
Ref country code: AT Ref legal event code: MK05 Ref document number: 1113177 Country of ref document: AT Kind code of ref document: T Effective date: 20190327 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: CZ Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20190327 Ref country code: ES Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20190327 Ref country code: RO Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20190327 Ref country code: IT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20190327 Ref country code: EE Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20190327 Ref country code: SK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20190327 Ref country code: AL Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20190327 Ref country code: PT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20190727 |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: PL |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: LU Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20190330 Ref country code: PL Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20190327 Ref country code: SM Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20190327 |
|
REG | Reference to a national code |
Ref country code: BE Ref legal event code: MM Effective date: 20190331 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: AT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20190327 Ref country code: IS Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20190727 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R097 Ref document number: 602016011663 Country of ref document: DE |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: MC Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20190327 Ref country code: DK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20190327 Ref country code: CH Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20190331 Ref country code: IE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20190330 Ref country code: LI Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20190331 |
|
PLBE | No opposition filed within time limit |
Free format text: ORIGINAL CODE: 0009261 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: SI Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20190327 Ref country code: BE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20190331 |
|
26N | No opposition filed |
Effective date: 20200103 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: TR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20190327 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: MT Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20190330 |
|
GBPC | Gb: european patent ceased through non-payment of renewal fee |
Effective date: 20200330 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: GB Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20200330 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: CY Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20190327 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: HU Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT; INVALID AB INITIO Effective date: 20160330 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: MK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20190327 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: FR Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20200331 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: DE Payment date: 20240206 Year of fee payment: 9 |