EP2753725B1 - Low density high strength steel and method for producing said steel - Google Patents
Low density high strength steel and method for producing said steel Download PDFInfo
- Publication number
- EP2753725B1 EP2753725B1 EP12704434.5A EP12704434A EP2753725B1 EP 2753725 B1 EP2753725 B1 EP 2753725B1 EP 12704434 A EP12704434 A EP 12704434A EP 2753725 B1 EP2753725 B1 EP 2753725B1
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- EP
- European Patent Office
- Prior art keywords
- steel sheet
- annealing
- steel
- strip
- temperature
- Prior art date
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- 229910000831 Steel Inorganic materials 0.000 title claims description 80
- 239000010959 steel Substances 0.000 title claims description 80
- 238000004519 manufacturing process Methods 0.000 title description 9
- 238000000137 annealing Methods 0.000 claims description 38
- 238000000034 method Methods 0.000 claims description 25
- 229910052782 aluminium Inorganic materials 0.000 claims description 19
- 229910001566 austenite Inorganic materials 0.000 claims description 16
- 229910052799 carbon Inorganic materials 0.000 claims description 15
- 229910052748 manganese Inorganic materials 0.000 claims description 14
- 238000005096 rolling process Methods 0.000 claims description 13
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 11
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 11
- 238000005097 cold rolling Methods 0.000 claims description 10
- 238000005098 hot rolling Methods 0.000 claims description 10
- 238000001953 recrystallisation Methods 0.000 claims description 10
- 230000009467 reduction Effects 0.000 claims description 10
- 230000000717 retained effect Effects 0.000 claims description 9
- 239000000203 mixture Substances 0.000 claims description 8
- 229910052759 nickel Inorganic materials 0.000 claims description 7
- 229910052710 silicon Inorganic materials 0.000 claims description 7
- 229910052719 titanium Inorganic materials 0.000 claims description 7
- 239000011247 coating layer Substances 0.000 claims description 6
- 239000010960 cold rolled steel Substances 0.000 claims description 6
- 229910052742 iron Inorganic materials 0.000 claims description 6
- 229910052804 chromium Inorganic materials 0.000 claims description 5
- 229910052802 copper Inorganic materials 0.000 claims description 5
- 238000011084 recovery Methods 0.000 claims description 5
- 229910018657 Mn—Al Inorganic materials 0.000 claims description 4
- 229910052796 boron Inorganic materials 0.000 claims description 4
- 229910052750 molybdenum Inorganic materials 0.000 claims description 4
- 238000003303 reheating Methods 0.000 claims description 4
- 229910052726 zirconium Inorganic materials 0.000 claims description 4
- 229910018134 Al-Mg Inorganic materials 0.000 claims description 3
- 229910018125 Al-Si Inorganic materials 0.000 claims description 3
- 229910018467 Al—Mg Inorganic materials 0.000 claims description 3
- 229910018464 Al—Mg—Si Inorganic materials 0.000 claims description 3
- 229910018520 Al—Si Inorganic materials 0.000 claims description 3
- 229910009369 Zn Mg Inorganic materials 0.000 claims description 3
- 229910007570 Zn-Al Inorganic materials 0.000 claims description 3
- 229910007573 Zn-Mg Inorganic materials 0.000 claims description 3
- 239000011248 coating agent Substances 0.000 claims description 3
- 238000000576 coating method Methods 0.000 claims description 3
- 239000012535 impurity Substances 0.000 claims description 3
- 239000000126 substance Substances 0.000 claims description 3
- 229910052721 tungsten Inorganic materials 0.000 claims description 3
- 229910052725 zinc Inorganic materials 0.000 claims description 3
- 239000004411 aluminium Substances 0.000 description 16
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 16
- 239000011572 manganese Substances 0.000 description 15
- 230000007423 decrease Effects 0.000 description 10
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 description 9
- 230000015572 biosynthetic process Effects 0.000 description 9
- PXHVJJICTQNCMI-UHFFFAOYSA-N nickel Substances [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 9
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 8
- 239000000463 material Substances 0.000 description 7
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical group [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 5
- 238000007792 addition Methods 0.000 description 5
- 238000005336 cracking Methods 0.000 description 5
- 230000005484 gravity Effects 0.000 description 5
- 239000010936 titanium Substances 0.000 description 5
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 4
- 239000011651 chromium Substances 0.000 description 4
- 229910052757 nitrogen Inorganic materials 0.000 description 4
- 239000002244 precipitate Substances 0.000 description 4
- 239000010703 silicon Substances 0.000 description 4
- 229910000859 α-Fe Inorganic materials 0.000 description 4
- OAICVXFJPJFONN-UHFFFAOYSA-N Phosphorus Chemical compound [P] OAICVXFJPJFONN-UHFFFAOYSA-N 0.000 description 3
- 229910052787 antimony Inorganic materials 0.000 description 3
- WATWJIUSRGPENY-UHFFFAOYSA-N antimony atom Chemical compound [Sb] WATWJIUSRGPENY-UHFFFAOYSA-N 0.000 description 3
- 239000010949 copper Substances 0.000 description 3
- 210000001787 dendrite Anatomy 0.000 description 3
- 230000000694 effects Effects 0.000 description 3
- 238000005246 galvanizing Methods 0.000 description 3
- 239000011159 matrix material Substances 0.000 description 3
- 150000001247 metal acetylides Chemical class 0.000 description 3
- 229910052698 phosphorus Inorganic materials 0.000 description 3
- 239000011574 phosphorus Substances 0.000 description 3
- 230000002829 reductive effect Effects 0.000 description 3
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 2
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 2
- NINIDFKCEFEMDL-UHFFFAOYSA-N Sulfur Chemical compound [S] NINIDFKCEFEMDL-UHFFFAOYSA-N 0.000 description 2
- 239000005864 Sulphur Substances 0.000 description 2
- 229910001567 cementite Inorganic materials 0.000 description 2
- 238000001816 cooling Methods 0.000 description 2
- 239000013078 crystal Substances 0.000 description 2
- 230000003247 decreasing effect Effects 0.000 description 2
- 230000007547 defect Effects 0.000 description 2
- 230000001419 dependent effect Effects 0.000 description 2
- 238000003618 dip coating Methods 0.000 description 2
- 239000006185 dispersion Substances 0.000 description 2
- KSOKAHYVTMZFBJ-UHFFFAOYSA-N iron;methane Chemical compound C.[Fe].[Fe].[Fe] KSOKAHYVTMZFBJ-UHFFFAOYSA-N 0.000 description 2
- -1 kappa carbide Inorganic materials 0.000 description 2
- 229910052751 metal Inorganic materials 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 229910052758 niobium Inorganic materials 0.000 description 2
- 239000010955 niobium Substances 0.000 description 2
- 238000001556 precipitation Methods 0.000 description 2
- 230000007704 transition Effects 0.000 description 2
- 229910052580 B4C Inorganic materials 0.000 description 1
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 description 1
- 229910017372 Fe3Al Inorganic materials 0.000 description 1
- 229910015372 FeAl Inorganic materials 0.000 description 1
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 1
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 1
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 description 1
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 description 1
- 230000002411 adverse Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- INAHAJYZKVIDIZ-UHFFFAOYSA-N boron carbide Chemical compound B12B3B4C32B41 INAHAJYZKVIDIZ-UHFFFAOYSA-N 0.000 description 1
- 238000004140 cleaning Methods 0.000 description 1
- 238000009749 continuous casting Methods 0.000 description 1
- 230000001186 cumulative effect Effects 0.000 description 1
- 230000001934 delay Effects 0.000 description 1
- 230000002542 deteriorative effect Effects 0.000 description 1
- 238000009713 electroplating Methods 0.000 description 1
- 239000012467 final product Substances 0.000 description 1
- 229910000765 intermetallic Inorganic materials 0.000 description 1
- 230000001788 irregular Effects 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 229910052749 magnesium Inorganic materials 0.000 description 1
- 239000011777 magnesium Substances 0.000 description 1
- 229910000734 martensite Inorganic materials 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 239000011733 molybdenum Substances 0.000 description 1
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 description 1
- 150000004767 nitrides Chemical class 0.000 description 1
- 230000036961 partial effect Effects 0.000 description 1
- 230000000704 physical effect Effects 0.000 description 1
- 238000005554 pickling Methods 0.000 description 1
- 230000002035 prolonged effect Effects 0.000 description 1
- 238000010791 quenching Methods 0.000 description 1
- 230000000171 quenching effect Effects 0.000 description 1
- 238000005204 segregation Methods 0.000 description 1
- 238000005507 spraying Methods 0.000 description 1
- 230000003019 stabilising effect Effects 0.000 description 1
- 230000003068 static effect Effects 0.000 description 1
- 238000005482 strain hardening Methods 0.000 description 1
- 238000005728 strengthening Methods 0.000 description 1
- 230000002277 temperature effect Effects 0.000 description 1
- 150000003568 thioethers Chemical class 0.000 description 1
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 1
- 239000010937 tungsten Substances 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
Classifications
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- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
- C21D8/0221—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the working steps
- C21D8/0236—Cold rolling
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- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
- C21D8/0221—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the working steps
- C21D8/0226—Hot rolling
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- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
- C21D8/0247—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the heat treatment
- C21D8/0263—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the heat treatment following hot rolling
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- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
- C21D8/04—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips to produce plates or strips for deep-drawing
- C21D8/041—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips to produce plates or strips for deep-drawing involving a particular fabrication or treatment of ingot or slab
- C21D8/0415—Rapid solidification; Thin strip casting
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- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
- C21D8/04—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips to produce plates or strips for deep-drawing
- C21D8/0421—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips to produce plates or strips for deep-drawing characterised by the working steps
- C21D8/0426—Hot rolling
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- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
- C21D8/04—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips to produce plates or strips for deep-drawing
- C21D8/0421—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips to produce plates or strips for deep-drawing characterised by the working steps
- C21D8/0436—Cold rolling
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- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
- C21D8/04—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips to produce plates or strips for deep-drawing
- C21D8/0447—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips to produce plates or strips for deep-drawing characterised by the heat treatment
- C21D8/0473—Final recrystallisation annealing
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- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D9/00—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
- C21D9/46—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for sheet metals
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- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/001—Ferrous alloys, e.g. steel alloys containing N
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- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/002—Ferrous alloys, e.g. steel alloys containing In, Mg, or other elements not provided for in one single group C22C38/001 - C22C38/60
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- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/02—Ferrous alloys, e.g. steel alloys containing silicon
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- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/04—Ferrous alloys, e.g. steel alloys containing manganese
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- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/06—Ferrous alloys, e.g. steel alloys containing aluminium
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- 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
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- 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
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- 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
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- 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
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- 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
- C22C38/20—Ferrous alloys, e.g. steel alloys containing chromium with copper
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- 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
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- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
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- C22C38/00—Ferrous alloys, e.g. steel alloys
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- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/32—Ferrous alloys, e.g. steel alloys containing chromium with boron
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- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/34—Ferrous alloys, e.g. steel alloys containing chromium with more than 1.5% by weight of silicon
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- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/38—Ferrous alloys, e.g. steel alloys containing chromium with more than 1.5% by weight of manganese
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- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
- C22C38/42—Ferrous alloys, e.g. steel alloys containing chromium with nickel with copper
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- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
- C22C38/44—Ferrous alloys, e.g. steel alloys containing chromium with nickel with molybdenum or tungsten
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- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
- C22C38/50—Ferrous alloys, e.g. steel alloys containing chromium with nickel with titanium or zirconium
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- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
- C22C38/54—Ferrous alloys, e.g. steel alloys containing chromium with nickel with boron
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- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
- C22C38/58—Ferrous alloys, e.g. steel alloys containing chromium with nickel with more than 1.5% by weight of manganese
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- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C2/00—Hot-dipping or immersion processes for applying the coating material in the molten state without affecting the shape; Apparatus therefor
- C23C2/02—Pretreatment of the material to be coated, e.g. for coating on selected surface areas
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- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C2/00—Hot-dipping or immersion processes for applying the coating material in the molten state without affecting the shape; Apparatus therefor
- C23C2/02—Pretreatment of the material to be coated, e.g. for coating on selected surface areas
- C23C2/022—Pretreatment of the material to be coated, e.g. for coating on selected surface areas by heating
- C23C2/0224—Two or more thermal pretreatments
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- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C2/00—Hot-dipping or immersion processes for applying the coating material in the molten state without affecting the shape; Apparatus therefor
- C23C2/02—Pretreatment of the material to be coated, e.g. for coating on selected surface areas
- C23C2/024—Pretreatment of the material to be coated, e.g. for coating on selected surface areas by cleaning or etching
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- C—CHEMISTRY; METALLURGY
- C25—ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
- C25D—PROCESSES FOR THE ELECTROLYTIC OR ELECTROPHORETIC PRODUCTION OF COATINGS; ELECTROFORMING; APPARATUS THEREFOR
- C25D5/00—Electroplating characterised by the process; Pretreatment or after-treatment of workpieces
- C25D5/34—Pretreatment of metallic surfaces to be electroplated
- C25D5/36—Pretreatment of metallic surfaces to be electroplated of iron or steel
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- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D1/00—General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
- C21D1/62—Quenching devices
- C21D1/673—Quenching devices for die quenching
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- C—CHEMISTRY; METALLURGY
- 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
- C21D2211/001—Austenite
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- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D2211/00—Microstructure comprising significant phases
- C21D2211/004—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
- C21D2211/005—Ferrite
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
- Y10T428/12736—Al-base component
- Y10T428/1275—Next to Group VIII or IB metal-base component
- Y10T428/12757—Fe
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
- Y10T428/12771—Transition metal-base component
- Y10T428/12785—Group IIB metal-base component
- Y10T428/12792—Zn-base component
- Y10T428/12799—Next to Fe-base component [e.g., galvanized]
Definitions
- the present invention relates to a low density and high strength steel sheet and to a method of producing a low density and high strength steel sheet, for instance for use as inner or outer steel sheets of a structural member for an automobile.
- steel Because of its excellent strength and ductility, and very low cost as compared to aluminium or magnesium, steel has been generally used to make a body of the automobile lighter by developing stronger grades which allow the use of thinner high strength steel sheet. However, in order to overcome a future limitation to the reduction in weight, it may be required to use alternative sources for reducing the weight of steel parts.
- TWIP steels with very high manganese contents of over 20% result in a lighter steel matrix.
- aluminium, as a lightweight element, is sometimes added so as to reduce the density of the steel. Additions of up to 15% aluminium have been used.
- a problem with the known steels is that processability in the existing facilities of the steel industry is problematic due to their proneness for cracking and their high deformation resistance during rolling. Other problems are weldability issues, particularly with the high aluminium content, and the likelihood of formation of undesirable martensite components.
- a low density and high strength steel sheet comprising 0.15% to 0.25% C, 2.5% to 4% Mn, 0.02% or less P, 0. 015% or less S, 6% to 9% Al and 0.01% or less N, the balance being iron and inevitable impurities, wherein 1.7 ⁇ (Mn-Al) + 52.7 ⁇ C is at least 3 and at most 4.5 as claimed in claim 1.
- Preferable embodiments are claimed in the dependent claims.
- composition of the present invention will be described in detail (all compositions in weight %).
- Carbon serves to create cementite (Fe,Mn) 3 C and kappa carbide (Fe,Mn) 3 AlC. Carbon is also an austenite stabilising element, and provides dispersion strengthening by forming precipitates. Particularly, since the columnar dendrite created during continuous casting is rapidly re-crystallized so as to create a coarse structure, the formation of carbides at high temperatures carbide is used to refine the structure. Additionally, the addition of carbon between 0.15 to 0.25% is used to increase the strength. However, if the added amount of carbon increases, the amounts of cementite and kappa carbide increase to contribute to an increase in strength, but greatly decrease ductility of steel.
- the carbon content is at least 0.16%, more preferably at least 0.17%.
- the carbon content is at most 0.23, more preferably at most 0.20%.
- Manganese contributes to the formation of austenite at high temperature, together with carbon. Further, manganese increases the lattice constant of steel thereby decreasing the density of the steel. A minimum amount of 2.5% of manganese was found to result in stable austenite and a significant decrease in density of the steel. However, if the amount of manganese is excessive, then the occurrence of central segregation results in an excessive band structure in a hot rolled sheet, which causes a decrease in ductility. The upper limit of manganese is therefore restricted to 4%. A preferable upper limit of manganese is 3.8%.
- Phosphorus is an element which is added in an amount as small as possible. It segregates on the grain boundary and causes hot shortness and cold shortness, so that workability of steel may be greatly reduced.
- the upper limit of phosphorus is restricted to 0.02%, but preferably the amount is limited to at most 0.01% or even 0.005%.
- sulphur promotes hot shortness. Particularly, it creates coarse MnS, which upon hot rolling and cold rolling, may causes a rolling plate to break, so that it is limited to 0.015% or less. Preferably the sulphur amount is limited to at most 0.01 % or even 0.005%.
- Aluminium is an important element in the present invention, together with carbon and manganese.
- the addition of aluminium decreases the density of the steel. Taking into consideration the decrease in specific gravity, it is preferred that a great quantity of Al be added.
- the addition of 6% aluminium or more results in a significant decrease in density of the steel.
- the amount of intermetallic compounds such as kappa carbide, FeAl or Fe 3 Al increases which causes a reduction of the ductility of steel, leading to cracking during cold rolling, so that the upper limit is restricted to 9%.
- aluminium causes an increase of the ductile-brittle transition temperature from sub-zero temperatures to around ambient temperatures. Therefore the upper aluminium limit is restricted to 9%.
- a preferable lower limit of aluminium is 6.2%.
- N Nitrogen causes the formation of AIN-precipitates if a great quantity of aluminium is added as in the present invention. These precipitates are effective in the refinement of columnar dendrite and the improvement in a ratio of equiaxed dendrite and for this reason a small amount of nitrogen in the steel is advantageous. However, large amounts of nitrogen cause large and amounts of potentially coarse AIN-precipitates which is undesirable. Thus, the upper limit of N is restricted to 0.01%. Preferably the nitrogen amount is limited to at most 0.008% or even 0.005%.
- composition of the steel sheet is chosen such that the value of (36 ⁇ C + Mn)/Al is at least 1.3 and at most 2.0.
- small to intermediate amounts of one or two or more elements of the group consisting of Si, Cr, Mo, Ni, Cu, B, Ti, Zr, Nb, Wand Ca may optionally be added.
- silicon Similar to aluminium, silicon also decreases the specific gravity of steel and contributes to the improvement in strength, but if being excessively added, it may create a thick, irregular high temperature oxide film on the surface of steel. Also, silicon causes a stronger increase of the ductile-brittle transition temperature from sub-zero temperatures to around ambient temperatures than aluminium. Therefore the upper silicon limit is restricted to 2%. Thus, it is preferred that the amount of silicon is within the range of 0.1 to 2.0%.
- Chromium is a ferrite-forming element which forms Cr-based carbides which may serve to refine the microstructure, so that the amount can be 0.1 % or more. However, if added too much, ductility is reduced, so that the upper limit is restricted to 0.3%.
- molybdenum is a ferrite-forming element which forms fine carbide, and is added by 0.05% or more. However, if excessively added, it decreases the ductility of steel, so that the upper limit thereof is restricted to 0.5%.
- Nickel is an austenite-forming element, which may introduces partial austenite during hot rolling to refine the structure, to thereby greatly improve the ridging resistibility.
- the price of nickel is high and increases the manufacturing cost, so that the limit is restricted to a range of 0.1 to 2.0%.
- Copper acts similar to nickel, but generally the price of copper is lower than that of nickel, so that it can be added in the range of 0.1 % or more. However, if excessively added, it exists on a grain boundary in a liquid state to cause intergranular brittleness, owing to fused metal, and causes edge cracking, so that the amount is restricted to a range of 0.1 to 1.0%.
- Boron restricts the recovery and recrystallization of ferrite in the process of hot rolling so as to contribute to the structure refinement thanks to cumulative rolling reduction and increase the strength of steel, so that the amount is 0.0005% or more.
- it may create boron-carbide, decreases the ductility of steel, and deteriorates the wettability of a hot-dipped galvanized coating layer, so that the upper limit is restricted to 0.003%.
- Titanium forms TiN or TiC or the like to thereby improve the grain refinement of the cast structure and contributes to the dispersion of kappa-carbide, so that it is added in the range of 0.01% or more.
- it is expensive and increases the manufacturing cost, and it reduces ductility due to the increase in strength through precipitation, so that the upper limit is restricted to 0.2%.
- Zirconium acts similar to titanium, and forms strong nitride and carbide relative to titanium, so that it is added in the range of 0.005% or more. However, it is expensive, so that the upper limit is restricted to 0.2%.
- Niobium acts similar to titanium, and thus it is added in the range of 0.005% or more. However, unlike titanium, it delays recrystallisation of the steel at high temperature to thereby greatly increase the rolling load of hot rolling. This may make it impossible to manufacture a thin steel sheet, so that the upper limit is restricted to 0.2%.
- Tungsten is a heavy element which increases the specific gravity of steel so the addition, if any is within a range of 0.05 to 1.0%.
- Antimony (Sb) segregates on the grain boundaries restricts the formation of kappa carbide so that antimony, if added, is added in the range of 0.005% or more. However, if excessively added, antimony segregates on a grain boundary to degrade ductility, so that the upper limit thereof is restricted to 0.2%.
- Ca forms sulphides such as CaS, and thereby prevents the formation of MnS, so that it is added in the range of 0.001 % or more to improve hot workability of steel.
- the upper limit is restricted to 0.2%.
- the steel sheet of the invention includes a retained austenite structure.
- the retained austenite complements the low strength of a ferrite matrix structure and also contributes to improvement in ductility thereof, so that it is included in the range of 5% or more by area.
- the upper limit thereof is preferably restricted to 20%, more preferably the upper limit is 15% or even 12%.
- a slab i.e. a thin slab ( ⁇ 150 mm), thick slab (150-400 mm) or cast strip ( ⁇ 20 mm)
- a slab is first heated in the temperature range of 1000 to 1250° C. If the reheating temperature exceeds 1250°C, coarse grains are formed in the slab, possibly creating ridging and hot shortness, whereas if it is below 1000°C, the finishing hot-rolling temperature becomes too low to both manufacture a steel sheet and remove an oxide film on a high temperature surface using the spraying of pressurized water, thereby causing surface defects.
- the reheating temperature is restricted to 1000 to 1250° C.
- the reheating temperature is at least 1100°C.
- the finishing rolling is implemented at a temperature of 900°C or less, preferably at most 850°C in order to refine crystal grains by dynamic or static recrystallisation during the hot rolling process.
- the material is subjected to the last hot deformation step while it is at least at the aforesaid temperature.
- the temperature is too low, hot deformation resistance increases to make it difficult to manufacture a steel sheet, and kappa carbide is precipitated to provide elongated structures, thereby increasing ridging defects, so that the rolling temperature is in the range of 700°C or more, preferably 750°C or more and more preferably 800°C or more.
- the hot-rolled steel strip is coiled at a temperature of 600°C or less. This temperature restricts the coarsening of the grain size and the excessive-precipitation of kappa carbide. It also reduces the risk of formation of abnormally coarsened grains caused by secondary recrystallisation of the coarse grains.
- the coiling temperature is below 550°C.
- the coiling temperature should be at least 200°C, and preferably at least 300°C, as quenching the material to ambient temperature proved to cause severe cracking during cold rolling.
- the resulting hot-rolled material can be manufactured into a hot-rolled steel sheet after being treated with pickling, and temper rolling and oiling.
- the steel sheet is a low density steel sheet having the specific gravity of 7400 kg/m 3 or less, preferably of 7300 kg/m 3 or less.
- the hot-rolled steel sheet can be manufactured into a cold rolled steel sheet after being pickled and cold rolled.
- cold rolling reduction is set to 40% or more. This is because, if the cold rolling reduction is set to 40% or more, stored energy by cold working can be secured, and a new recrystallised structure can be obtained.
- the minimum cold rolling reduction is 50%.
- the upper limit thereof is restricted to 90% or less in consideration of production efficiency and economy.
- the material may be subjected to intermediate annealing in between cold rolling reductions or steps.
- the cold rolled steel sheet is treated with continuous annealing or continuous hot-dip galvanizing after cleaning the surface if necessary.
- the annealing rate is preferably selected in the range of 1 °C/s to 20°C/s. If the annealing rate is less than 1°C/s, productivity is too low, and the steel sheet is exposed to high temperature condition for a long time to thereby cause the coarsening of crystal grains and reduction in strength, deteriorating the quality of material. On the other hand, if the annealing rate exceeds 20° C/s, because of insufficient re-melting of carbide, the formation of austenite also becomes insufficient and thus retained austenite is reduced to thereby reduce the ductility.
- the cooling rate after annealing is preferably between 10 and 50°C/s, either to ambient temperatures, or to the galvanising bath and/or the overaging treatment. After galvanising or overageing, the cooling rate is preferably between 10 and 50°C/s, more preferably between 10 and 25°C/s,
- Annealing is implemented in the temperature range between the recovery temperature and 900° C. Between the recovery temperature and below the recrystallisation temperature, some ductility is recovered. This may be used to create high strength steels whilst securing adequate ductility by selecting the recovery annealing temperature and time. Above the recrystallisation temperature and below 900°C, the cold deformed structure readily recrystallises. The combination of annealing temperature and annealing time to obtain full recrystallisation of the cold-rolled steel strip can be easily determined. The inventors found a lower austenite content in the final product after annealing if the cold-rolled material was annealed at a higher annealing temperature.
- the lower limit is at least 800°C
- the annealing is carried out for 10 seconds or more so as to achieve excellent strength and workability. However, if the annealing time exceeds 180 seconds, the productivity is excessively lowered and the properties may be adversely affected by the prolonged annealing process.
- the steel sheet After annealing the steel sheet is cooled to the temperature of the bath and may be coated with Zn, Zn-Fe, Zn-Al, Zn-Mg, Zn-Al-Mg, Al-Si, Al-Mg-Si, or the like in the thickness of 10 to 200 ⁇ m per one side thereof, thereby forming coated steel sheet, by a hot dip coating process.
- These or other metal coating layers may also be applied by an electroplating process.
- the coating thickness on the or each surface is between 10 ⁇ m and 200 ⁇ m.
- the material is subjected to overageing after annealing. If applicable this overageing may precede or follow after the hot dip coating process, depending on the lay-out of the plant or depending on metallurgical preferences.
- the overageing temperature is preferably between 350 and 500°C, and preferably about 400°C.
- the overageing time is preferably at least 30 and/or at most 180s.
- the annealing temperature is preferably at least 825°C and/or preferably at most 875°C.
- the steel sheet produced as above carbides and 5% or more of retained austenite is dispersed in a ferrite matrix, so that the tensile strength is high in the level of 600 to 900 MPa, the ductility is excellent, and therefore the combination of strength-ductility is also excellent.
- the steel sheet has a tensile strength of 600 to 900MPa.
- the steels were then subjected to cold-rolling at a reduction (CRR) of 67% and continuously annealed at annealing temperatures (AT) between 800 and 1050°C (see Table 3) and with and without overageing at 400°C (see Table 4).
- the annealing time was 60 seconds and the overageing time was 80 seconds.
- the overageing treatment appears to have a beneficial effect in combination with a higher annealing temperature.
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Description
- The present invention relates to a low density and high strength steel sheet and to a method of producing a low density and high strength steel sheet, for instance for use as inner or outer steel sheets of a structural member for an automobile.
- Because of its excellent strength and ductility, and very low cost as compared to aluminium or magnesium, steel has been generally used to make a body of the automobile lighter by developing stronger grades which allow the use of thinner high strength steel sheet. However, in order to overcome a future limitation to the reduction in weight, it may be required to use alternative sources for reducing the weight of steel parts.
- Steels with lower density are known in the art. TWIP steels with very high manganese contents of over 20% result in a lighter steel matrix. Also aluminium, as a lightweight element, is sometimes added so as to reduce the density of the steel. Additions of up to 15% aluminium have been used.
- Such a steel is disclosed in
JP 2005 015 909 - A problem with the known steels is that processability in the existing facilities of the steel industry is problematic due to their proneness for cracking and their high deformation resistance during rolling. Other problems are weldability issues, particularly with the high aluminium content, and the likelihood of formation of undesirable martensite components.
- It is an object of the invention to provide a low density and high strength steel sheet which can be produced using existing facilities of the steel industry.
- It is also an object of the invention to provide a relatively low alloyed low density and high strength steel sheet which has a strength of at least 600 MPa.
- It is also an object of the invention to provide a process for producing a low density and high strength steel sheet.
- One or more of these objects are reached by providing a low density and high strength steel sheet comprising 0.15% to 0.25% C, 2.5% to 4% Mn, 0.02% or less P, 0. 015% or less S, 6% to 9% Al and 0.01% or less N, the balance being iron and inevitable impurities, wherein 1.7·(Mn-Al) + 52.7·C is at least 3 and at most 4.5 as claimed in claim 1. Preferable embodiments are claimed in the dependent claims.
- One or more of these objects are reached by the process of claim 7. Preferable embodiments of the process are claimed in the dependent claims.
- Hereinafter, the composition of the present invention will be described in detail (all compositions in weight %).
- Carbon serves to create cementite (Fe,Mn)3C and kappa carbide (Fe,Mn)3AlC. Carbon is also an austenite stabilising element, and provides dispersion strengthening by forming precipitates. Particularly, since the columnar dendrite created during continuous casting is rapidly re-crystallized so as to create a coarse structure, the formation of carbides at high temperatures carbide is used to refine the structure. Additionally, the addition of carbon between 0.15 to 0.25% is used to increase the strength. However, if the added amount of carbon increases, the amounts of cementite and kappa carbide increase to contribute to an increase in strength, but greatly decrease ductility of steel. In the steel to which aluminium is added, particular, kappa carbide is precipitated on a grain boundary of ferrite to cause brittleness. Values below 0.15% result in too low a strength and values higher than 0.25% tends to increase the risk of welding related issues, so that the carbon content is maximised to 0.25. Preferably, the carbon content is at least 0.16%, more preferably at least 0.17%. Preferably, the carbon content is at most 0.23, more preferably at most 0.20%.
- Manganese contributes to the formation of austenite at high temperature, together with carbon. Further, manganese increases the lattice constant of steel thereby decreasing the density of the steel. A minimum amount of 2.5% of manganese was found to result in stable austenite and a significant decrease in density of the steel. However, if the amount of manganese is excessive, then the occurrence of central segregation results in an excessive band structure in a hot rolled sheet, which causes a decrease in ductility. The upper limit of manganese is therefore restricted to 4%. A preferable upper limit of manganese is 3.8%.
- Phosphorus is an element which is added in an amount as small as possible. It segregates on the grain boundary and causes hot shortness and cold shortness, so that workability of steel may be greatly reduced. The upper limit of phosphorus is restricted to 0.02%, but preferably the amount is limited to at most 0.01% or even 0.005%.
- Similar to phosphorus, sulphur promotes hot shortness. Particularly, it creates coarse MnS, which upon hot rolling and cold rolling, may causes a rolling plate to break, so that it is limited to 0.015% or less. Preferably the sulphur amount is limited to at most 0.01 % or even 0.005%.
- Aluminium is an important element in the present invention, together with carbon and manganese. The addition of aluminium decreases the density of the steel. Taking into consideration the decrease in specific gravity, it is preferred that a great quantity of Al be added. The addition of 6% aluminium or more results in a significant decrease in density of the steel. However, if aluminium is excessively added, the amount of intermetallic compounds such as kappa carbide, FeAl or Fe3Al increases which causes a reduction of the ductility of steel, leading to cracking during cold rolling, so that the upper limit is restricted to 9%. Also, aluminium causes an increase of the ductile-brittle transition temperature from sub-zero temperatures to around ambient temperatures. Therefore the upper aluminium limit is restricted to 9%. A preferable lower limit of aluminium is 6.2%.
- Nitrogen causes the formation of AIN-precipitates if a great quantity of aluminium is added as in the present invention. These precipitates are effective in the refinement of columnar dendrite and the improvement in a ratio of equiaxed dendrite and for this reason a small amount of nitrogen in the steel is advantageous. However, large amounts of nitrogen cause large and amounts of potentially coarse AIN-precipitates which is undesirable. Thus, the upper limit of N is restricted to 0.01%. Preferably the nitrogen amount is limited to at most 0.008% or even 0.005%.
- The inventors found that a steel within the boundaries of the chemical composition as explained hereinabove did not always result in a steel that performed satisfactorily. The ductility of the obtained sheet appeared to be too low if the outcome of the equation (1.7 x (Mn-Al) + 52.7C) is lower than 3 or higher than 4.5.
- By this equation the amount of manganese and carbon is controlled in relation to the amount of aluminium in order to control the ductility.
- In an embodiment the composition of the steel sheet is chosen such that the value of (36·C + Mn)/Al is at least 1.3 and at most 2.0.
- In addition to the above basic composition of the present invention, in order to improve or compensate the strength, ductility, and the other physical properties of steel, small to intermediate amounts of one or two or more elements of the group consisting of Si, Cr, Mo, Ni, Cu, B, Ti, Zr, Nb, Wand Ca may optionally be added.
- Similar to aluminium, silicon also decreases the specific gravity of steel and contributes to the improvement in strength, but if being excessively added, it may create a thick, irregular high temperature oxide film on the surface of steel. Also, silicon causes a stronger increase of the ductile-brittle transition temperature from sub-zero temperatures to around ambient temperatures than aluminium. Therefore the upper silicon limit is restricted to 2%. Thus, it is preferred that the amount of silicon is within the range of 0.1 to 2.0%.
- Chromium is a ferrite-forming element which forms Cr-based carbides which may serve to refine the microstructure, so that the amount can be 0.1 % or more. However, if added too much, ductility is reduced, so that the upper limit is restricted to 0.3%.
- Similar to chromium, molybdenum is a ferrite-forming element which forms fine carbide, and is added by 0.05% or more. However, if excessively added, it decreases the ductility of steel, so that the upper limit thereof is restricted to 0.5%.
- Nickel is an austenite-forming element, which may introduces partial austenite during hot rolling to refine the structure, to thereby greatly improve the ridging resistibility. However, the price of nickel is high and increases the manufacturing cost, so that the limit is restricted to a range of 0.1 to 2.0%.
- Copper acts similar to nickel, but generally the price of copper is lower than that of nickel, so that it can be added in the range of 0.1 % or more. However, if excessively added, it exists on a grain boundary in a liquid state to cause intergranular brittleness, owing to fused metal, and causes edge cracking, so that the amount is restricted to a range of 0.1 to 1.0%.
- Boron restricts the recovery and recrystallization of ferrite in the process of hot rolling so as to contribute to the structure refinement thanks to cumulative rolling reduction and increase the strength of steel, so that the amount is 0.0005% or more. However, if excessively added, it may create boron-carbide, decreases the ductility of steel, and deteriorates the wettability of a hot-dipped galvanized coating layer, so that the upper limit is restricted to 0.003%.
- Titanium forms TiN or TiC or the like to thereby improve the grain refinement of the cast structure and contributes to the dispersion of kappa-carbide, so that it is added in the range of 0.01% or more. However, it is expensive and increases the manufacturing cost, and it reduces ductility due to the increase in strength through precipitation, so that the upper limit is restricted to 0.2%.
- Zirconium acts similar to titanium, and forms strong nitride and carbide relative to titanium, so that it is added in the range of 0.005% or more. However, it is expensive, so that the upper limit is restricted to 0.2%.
- Niobium acts similar to titanium, and thus it is added in the range of 0.005% or more. However, unlike titanium, it delays recrystallisation of the steel at high temperature to thereby greatly increase the rolling load of hot rolling. This may make it impossible to manufacture a thin steel sheet, so that the upper limit is restricted to 0.2%.
- Tungsten is a heavy element which increases the specific gravity of steel so the addition, if any is within a range of 0.05 to 1.0%. Antimony (Sb) segregates on the grain boundaries restricts the formation of kappa carbide so that antimony, if added, is added in the range of 0.005% or more. However, if excessively added, antimony segregates on a grain boundary to degrade ductility, so that the upper limit thereof is restricted to 0.2%.
- Ca forms sulphides such as CaS, and thereby prevents the formation of MnS, so that it is added in the range of 0.001 % or more to improve hot workability of steel. The upper limit is restricted to 0.2%.
- The steel sheet of the invention includes a retained austenite structure. The retained austenite complements the low strength of a ferrite matrix structure and also contributes to improvement in ductility thereof, so that it is included in the range of 5% or more by area. The upper limit thereof is preferably restricted to 20%, more preferably the upper limit is 15% or even 12%.
- Hereinafter, a manufacturing method of the high strength and low specific gravity steel sheet will be described in detail.
- In order to manufacture the steel sheet of the invention, a slab (i.e. a thin slab (<150 mm), thick slab (150-400 mm) or cast strip (<20 mm)) is first heated in the temperature range of 1000 to 1250° C. If the reheating temperature exceeds 1250°C, coarse grains are formed in the slab, possibly creating ridging and hot shortness, whereas if it is below 1000°C, the finishing hot-rolling temperature becomes too low to both manufacture a steel sheet and remove an oxide film on a high temperature surface using the spraying of pressurized water, thereby causing surface defects. Thus, the reheating temperature is restricted to 1000 to 1250° C. Preferably the reheating temperature is at least 1100°C.
- Since the hot rolling is implemented at a temperature as low as possible so as to effectively obtain fine grains, according to the present invention, the finishing rolling is implemented at a temperature of 900°C or less, preferably at most 850°C in order to refine crystal grains by dynamic or static recrystallisation during the hot rolling process. This means that the material is subjected to the last hot deformation step while it is at least at the aforesaid temperature. However, if the temperature is too low, hot deformation resistance increases to make it difficult to manufacture a steel sheet, and kappa carbide is precipitated to provide elongated structures, thereby increasing ridging defects, so that the rolling temperature is in the range of 700°C or more, preferably 750°C or more and more preferably 800°C or more.
- The hot-rolled steel strip is coiled at a temperature of 600°C or less. This temperature restricts the coarsening of the grain size and the excessive-precipitation of kappa carbide. It also reduces the risk of formation of abnormally coarsened grains caused by secondary recrystallisation of the coarse grains. Preferably the coiling temperature is below 550°C. The coiling temperature should be at least 200°C, and preferably at least 300°C, as quenching the material to ambient temperature proved to cause severe cracking during cold rolling.
- The resulting hot-rolled material can be manufactured into a hot-rolled steel sheet after being treated with pickling, and temper rolling and oiling. According to the present invention, the steel sheet is a low density steel sheet having the specific gravity of 7400 kg/m3 or less, preferably of 7300 kg/m3 or less.
- Further, the hot-rolled steel sheet can be manufactured into a cold rolled steel sheet after being pickled and cold rolled.
- In the cold rolling, cold rolling reduction is set to 40% or more. This is because, if the cold rolling reduction is set to 40% or more, stored energy by cold working can be secured, and a new recrystallised structure can be obtained. Preferably the minimum cold rolling reduction is 50%. However, the upper limit thereof is restricted to 90% or less in consideration of production efficiency and economy. Optionally, the material may be subjected to intermediate annealing in between cold rolling reductions or steps.
- The cold rolled steel sheet is treated with continuous annealing or continuous hot-dip galvanizing after cleaning the surface if necessary. The annealing rate is preferably selected in the range of 1 °C/s to 20°C/s. If the annealing rate is less than 1°C/s, productivity is too low, and the steel sheet is exposed to high temperature condition for a long time to thereby cause the coarsening of crystal grains and reduction in strength, deteriorating the quality of material. On the other hand, if the annealing rate exceeds 20° C/s, because of insufficient re-melting of carbide, the formation of austenite also becomes insufficient and thus retained austenite is reduced to thereby reduce the ductility. The cooling rate after annealing is preferably between 10 and 50°C/s, either to ambient temperatures, or to the galvanising bath and/or the overaging treatment. After galvanising or overageing, the cooling rate is preferably between 10 and 50°C/s, more preferably between 10 and 25°C/s,
- Annealing is implemented in the temperature range between the recovery temperature and 900° C. Between the recovery temperature and below the recrystallisation temperature, some ductility is recovered. This may be used to create high strength steels whilst securing adequate ductility by selecting the recovery annealing temperature and time. Above the recrystallisation temperature and below 900°C, the cold deformed structure readily recrystallises. The combination of annealing temperature and annealing time to obtain full recrystallisation of the cold-rolled steel strip can be easily determined. The inventors found a lower austenite content in the final product after annealing if the cold-rolled material was annealed at a higher annealing temperature. Above 900°C, because of the formation of a lower amount of austenite, the ductility decreases. A suitable lower limit for the annealing temperature in the case where the annealed steel was found to be 750 °C. Preferably the lower limit is at least 800°C The annealing is carried out for 10 seconds or more so as to achieve excellent strength and workability. However, if the annealing time exceeds 180 seconds, the productivity is excessively lowered and the properties may be adversely affected by the prolonged annealing process.
- After annealing the steel sheet is cooled to the temperature of the bath and may be coated with Zn, Zn-Fe, Zn-Al, Zn-Mg, Zn-Al-Mg, Al-Si, Al-Mg-Si, or the like in the thickness of 10 to 200 µm per one side thereof, thereby forming coated steel sheet, by a hot dip coating process. These or other metal coating layers may also be applied by an electroplating process. Preferably the coating thickness on the or each surface is between 10 µm and 200 µm.
- Preferably the material is subjected to overageing after annealing. If applicable this overageing may precede or follow after the hot dip coating process, depending on the lay-out of the plant or depending on metallurgical preferences. The overageing temperature is preferably between 350 and 500°C, and preferably about 400°C. The overageing time is preferably at least 30 and/or at most 180s. In case of such an overageing treatment, the annealing temperature is preferably at least 825°C and/or preferably at most 875°C.
- In the steel sheet produced as above, carbides and 5% or more of retained austenite is dispersed in a ferrite matrix, so that the tensile strength is high in the level of 600 to 900 MPa, the ductility is excellent, and therefore the combination of strength-ductility is also excellent. In a preferable embodiment the steel sheet has a tensile strength of 600 to 900MPa.
- The present invention will now be described in detail with reference to the following examples. The examples are for illustrative purposes, and are not intended to restrict the scope of the present invention in any way.
- Steel slabs having compositions shown in Table 1 were produced, reheated at 1200°C (RHT), and hot rolled at a finish rolling temperature of 900°C. The thickness of the hot-rolled steel sheet was 3 mm, and the hot-rolled steel sheet was coiled at a temperature (CT) of 400°C or 650°C (S3) (See Table 2). The inventors found that finish hot rolling at lower temperatures (but above 700°C) such as 850°C did not affect the microstructure or properties of the steel, but only had an effect on the rolling forces which increase with decreasing rolling temperatures. However, these increased rolling forces can be easily overcome by using a rolling mill of adequate power.
- The steels were then subjected to cold-rolling at a reduction (CRR) of 67% and continuously annealed at annealing temperatures (AT) between 800 and 1050°C (see Table 3) and with and without overageing at 400°C (see Table 4). The annealing time was 60 seconds and the overageing time was 80 seconds.
Table 1 - Chemical composition No. C Al Mn Si P S N 1.7*(Mn - Al) + 52.7*C S1 0.18 6.7 3.4 0.01 0.004 0.003 0.005 3.90 S2 0.13 9.1 5.4 0.01 0.003 0.004 0.006 0.60 S3 0.004 6.8 0.02 0.01 0.004 0.005 0.004 -11.30 S1* 0.17 7.0 3.6 0.01 0.004 0.003 0.004 3.18 S1** 0.19 8.0 3.9 0.01 0.004 0.003 0.005 3.05 Table 2 - Process parameters and mechanical properties (YS: yield strength in MPa, TS: tensile strength in MPa, EI: elongation in %, RA: retained austenite in vol.%) Type RHT (°C) CT (°C) CRR (%) AT (°C) YS (MPa) TS (MPa) EI (%) RA (%) Cracking S1 1200 400 67 850 466 626 21 8 no S2 1200 400 67 850 445 675 4.5 2.5 yes S3 1200 650 67 850 342 465 31 0 no Table 3 - Effect of annealing temperature effect without overageing Type RHT (°C) CT (°C) CRR (%) AT (°C) YS (MPa) TS (MPa) EI (%) RA (%) S1 1200 400 67 800 489 652 23 10 S1 1200 400 67 850 466 626 21 8 S1 1200 400 67 900 435 652 14 6 S1 1200 400 67 1050 401 670 8 4 Table 4 - Effect of combination of annealing temperature and overaging temperature Type AT (°C) OT (°C) YS (MPa) TS (MPa) EI (%) S1 800 no 489 652 23 S1 800 400 489 651 23 S1 850 no 466 626 21 S1 850 400 467 631 28 - Results with steels S1* and S1** were similar to those of S1 when processed like S1.
- It is clear that there is always a balance between recrystallisation during annealing and the amount of retained austenite. The higher the annealing temperature, the lower the amount of retained austenite.
- The overageing treatment appears to have a beneficial effect in combination with a higher annealing temperature.
Claims (15)
- A low density high strength steel sheet comprising 0.15% to 0.25% C, 2.5% to 4% Mn, 0.02% or less P, 0. 015% or less S, 6% to 9% Al and 0.01% or less N, optionally comprising one or two or more elements selected from the group consisting of 0.1% to 2.0% Si, 0.1% to 0.3% Cr, 0.05% to 0.5% Mo, 0.1% to 2.0% Ni, 0.1% to 1.0% Cu, 0.0005% to 0.003% B, 0.01% to 0.2% Ti, 0.005% to 0.2% Zr, 0.05% to 1.0% W, 0.001% to 0.2% Ca, the balance being iron and inevitable impurities, wherein 1.7·(Mn-Al) + 52.7·C is at least 3 and at most 4.5.
- The steel sheet according to claim 1 wherein the amount of retained austenite in the sheet is 5% or more.
- The steel sheet according to claim 1 or 2, wherein the carbon content is at most 0.23%.
- The steel sheet according to any one of claims 1 to 3 wherein the density of the steel sheet is at most 7400 kg/m3, preferably at most 7300 kg/m3, preferably wherein the steel sheet has a tensile strength of 600 to 900MPa.
- The steel sheet according to any one of claims 1 to 4 wherein a coating layer is provided on one or both of the major surfaces wherein the coating layer is selected from Zn, Zn-Fe, Zn-Al, Zn-Mg, Zn-Al-Mg, Al-Si, and Al-Mg-Si and wherein the coating thickness on the or each major surface is between 10 µm and 200 µm.
- The steel sheet according to any one of claims 1 to 5 wherein the value of (36·C + Mn)/Al is at least 1.3 and at most 2.0.
- A process for producing a low density high strength steel sheet comprising 0.15% to 0.25% C, 2.5% to 4% Mn, 0.02% or less P, 0. 015% or less S, 6% to 9% Al and 0.01% or less N, optionally comprising one or two or more elements selected from the group consisting of 0.1% to 2.0% Si, 0.1% to 0.3% Cr, 0.05% to 0.5% Mo, 0.1% to 2.0% Ni, 0.1% to 1.0% Cu, 0.0005% to 0.003% B, 0.01% to 0.2% Ti, 0.005% to 0.2% Zr, 0.1% to 1.0% W, and 0.001% to 0.2% Ca, the balance being iron and inevitable impurities, wherein 1.7·(Mn-Al) + 52.7·C is at least 3 and at most 4.5, the process comprising the steps of:- providing a steel slab, thin slab or strip having the said chemical composition;- preparing the said slab or strip for hot rolling by reheating it within a range of from 1000°C to 1250°C;- subjecting the slab or strip to the last finishing hot-rolling step while the rolled strip has a temperature of between 700°C and 900°C;- coiling the hot-rolled strip at 600°C or less.
- Process according to claim 7, the process further comprising the steps of:- cold-rolling the hot-rolled steel slab or strip at a rolling reduction of 40% to 90% to produce a cold-rolled steel strip;- continuously annealing the cold-rolled steel strip at a maximum temperature of 900°C at an annealing rate of 1 to 20°C/s for 10 to 180 seconds.
- Process for producing a low density and high strength steel sheet according to claim 8 wherein the continuous annealing process is a recovery annealing.
- Process for producing a low density and high strength steel sheet according to claim 8 wherein the continuous annealing process is a recrystallisation annealing.
- Process according to any one of claims 7 to 10 wherein the amount of retained austenite in the steel sheet is 5% or more.
- Process according to any one of claims 7 to 11 wherein the value of (36·C + Mn)/Al is at least 1.3 and at most 2.0.
- Process according to any one of claims 8 to 12 , wherein after the annealing process a coating layer is provided on one or both of the major surfaces wherein the coating layer is selected from Zn, Zn-Fe, Zn-Al, Zn-Mg, Zn-Al-Mg, Al-Si, and Al-Mg-Si, preferably wherein the coating thickness on the or each major surface is between 10 µm and 200 µm.
- Process according to any one of claims 8 to 13 wherein the annealing process includes an overageing step, preferably at a temperature between 350 and 500°C and preferably for a period of between 30 to 180 seconds, preferably wherein the annealing temperature is at least 825°C and/or at most 875°C.
- Process according to any one of claims 8 to 14 wherein the combination of annealing temperature and annealing time is sufficient to obtain full recrystallisation of the cold-rolled steel strip, preferably wherein the annealing temperature is 750°C or more.
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CN109440017A (en) | 2013-05-01 | 2019-03-08 | 新日铁住金株式会社 | The excellent high-intensitive low-gravity steel plate of spot weldability |
WO2014178358A1 (en) * | 2013-05-01 | 2014-11-06 | 新日鐵住金株式会社 | Galvanized steel sheet and production method therefor |
KR101560940B1 (en) | 2013-12-24 | 2015-10-15 | 주식회사 포스코 | Light weight steel sheet having excellent strength and ductility |
CN104789902A (en) * | 2015-03-20 | 2015-07-22 | 苏州科胜仓储物流设备有限公司 | High-strength steel plate for steel platform and forging technology thereof |
CN104789888A (en) * | 2015-03-20 | 2015-07-22 | 苏州科胜仓储物流设备有限公司 | High strength steel sheet for middle-sized storage rack and forging technology of high strength steel sheet |
CN104789901A (en) * | 2015-03-20 | 2015-07-22 | 苏州科胜仓储物流设备有限公司 | High strength steel sheet for heavy mold storage rack and heat treatment technology of high strength steel sheet |
CN104789903A (en) * | 2015-03-20 | 2015-07-22 | 苏州科胜仓储物流设备有限公司 | High strength steel sheet for heavy cross beam storage rack and heat treatment technology of high strength steel sheet |
CN104789904A (en) * | 2015-03-20 | 2015-07-22 | 苏州科胜仓储物流设备有限公司 | High strength steel sheet for light mold shelf and heat treatment technology of high strength steel sheet |
CN106011652B (en) * | 2016-06-28 | 2017-12-26 | 宝山钢铁股份有限公司 | A kind of excellent cold rolling low-density steel plate of phosphorus characteristic and its manufacture method |
UA124357C2 (en) * | 2016-12-22 | 2021-09-01 | Арселорміттал | Cold rolled and heat treated steel sheet, method of production thereof and use of such steel to produce vehicle parts |
CN107326282B (en) * | 2017-07-13 | 2018-09-14 | 武汉钢铁有限公司 | 600MPa grades of high-yield-ratio hot rolling high-strength light steel and its manufacturing method |
WO2019122960A1 (en) * | 2017-12-19 | 2019-06-27 | Arcelormittal | Cold rolled and heat treated steel sheet, method of production thereof and use of such steel to produce vehicle parts |
CN108950392B (en) * | 2018-07-19 | 2020-10-30 | 首钢集团有限公司 | Ultrahigh-ductility low-density steel and preparation method thereof |
CN113430453A (en) * | 2021-05-27 | 2021-09-24 | 南京钢铁股份有限公司 | Preparation method of low-density composite steel plate |
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JP3598087B2 (en) * | 2001-10-01 | 2004-12-08 | 新日本製鐵株式会社 | High-strength galvannealed steel sheet with excellent workability and method for producing the same |
JP3828845B2 (en) * | 2002-08-07 | 2006-10-04 | 新日本製鐵株式会社 | Steel with excellent machinability and wet corrosion resistance |
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