WO2018159405A1 - 高強度鋼板およびその製造方法 - Google Patents
高強度鋼板およびその製造方法 Download PDFInfo
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- WO2018159405A1 WO2018159405A1 PCT/JP2018/006173 JP2018006173W WO2018159405A1 WO 2018159405 A1 WO2018159405 A1 WO 2018159405A1 JP 2018006173 W JP2018006173 W JP 2018006173W WO 2018159405 A1 WO2018159405 A1 WO 2018159405A1
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- steel sheet
- less
- phase
- strength steel
- martensite
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- 229910000831 Steel Inorganic materials 0.000 title claims abstract description 74
- 239000010959 steel Substances 0.000 title claims abstract description 74
- 238000004519 manufacturing process Methods 0.000 title claims abstract description 20
- 229910000734 martensite Inorganic materials 0.000 claims abstract description 63
- 229910000859 α-Fe Inorganic materials 0.000 claims abstract description 35
- 239000002245 particle Substances 0.000 claims abstract description 33
- 238000005096 rolling process Methods 0.000 claims abstract description 20
- 239000000203 mixture Substances 0.000 claims abstract description 19
- 238000000137 annealing Methods 0.000 claims description 33
- 238000005452 bending Methods 0.000 claims description 19
- 229910001563 bainite Inorganic materials 0.000 claims description 16
- 238000001816 cooling Methods 0.000 claims description 16
- 238000007747 plating Methods 0.000 claims description 16
- 239000010960 cold rolled steel Substances 0.000 claims description 9
- 238000010438 heat treatment Methods 0.000 claims description 9
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 6
- 238000005246 galvanizing Methods 0.000 claims description 6
- 239000012535 impurity Substances 0.000 claims description 4
- 229910052718 tin Inorganic materials 0.000 claims description 4
- 229910052787 antimony Inorganic materials 0.000 claims description 3
- 229910052785 arsenic Inorganic materials 0.000 claims description 3
- 229910052792 caesium Inorganic materials 0.000 claims description 3
- 229910052791 calcium Inorganic materials 0.000 claims description 3
- 229910052804 chromium Inorganic materials 0.000 claims description 3
- 229910052802 copper Inorganic materials 0.000 claims description 3
- 229910052735 hafnium Inorganic materials 0.000 claims description 3
- 229910052745 lead Inorganic materials 0.000 claims description 3
- 229910052749 magnesium Inorganic materials 0.000 claims description 3
- 229910052759 nickel Inorganic materials 0.000 claims description 3
- 229910052758 niobium Inorganic materials 0.000 claims description 3
- 229910052761 rare earth metal Inorganic materials 0.000 claims description 3
- 229910052712 strontium Inorganic materials 0.000 claims description 3
- 229910052715 tantalum Inorganic materials 0.000 claims description 3
- 229910052721 tungsten Inorganic materials 0.000 claims description 3
- 229910052720 vanadium Inorganic materials 0.000 claims description 3
- 229910052725 zinc Inorganic materials 0.000 claims description 3
- 229910052742 iron Inorganic materials 0.000 claims description 2
- 239000000463 material Substances 0.000 abstract description 42
- 238000000034 method Methods 0.000 description 22
- 229910001566 austenite Inorganic materials 0.000 description 18
- 230000000694 effects Effects 0.000 description 15
- 229910001567 cementite Inorganic materials 0.000 description 10
- 230000000717 retained effect Effects 0.000 description 10
- KSOKAHYVTMZFBJ-UHFFFAOYSA-N iron;methane Chemical compound C.[Fe].[Fe].[Fe] KSOKAHYVTMZFBJ-UHFFFAOYSA-N 0.000 description 9
- 238000005260 corrosion Methods 0.000 description 8
- 230000007797 corrosion Effects 0.000 description 8
- 230000007423 decrease Effects 0.000 description 8
- 238000005098 hot rolling Methods 0.000 description 6
- 238000005097 cold rolling Methods 0.000 description 5
- 238000005275 alloying Methods 0.000 description 4
- 150000001247 metal acetylides Chemical class 0.000 description 4
- 230000006911 nucleation Effects 0.000 description 4
- 238000010899 nucleation Methods 0.000 description 4
- 230000005855 radiation Effects 0.000 description 4
- 238000012360 testing method Methods 0.000 description 4
- 230000009466 transformation Effects 0.000 description 4
- 230000015572 biosynthetic process Effects 0.000 description 3
- 238000005266 casting Methods 0.000 description 3
- 238000005520 cutting process Methods 0.000 description 3
- 238000005259 measurement Methods 0.000 description 3
- 238000002844 melting Methods 0.000 description 3
- 230000008018 melting Effects 0.000 description 3
- 229910001562 pearlite Inorganic materials 0.000 description 3
- 238000005204 segregation Methods 0.000 description 3
- 238000005728 strengthening Methods 0.000 description 3
- CURLTUGMZLYLDI-UHFFFAOYSA-N Carbon dioxide Chemical compound O=C=O CURLTUGMZLYLDI-UHFFFAOYSA-N 0.000 description 2
- 238000002441 X-ray diffraction Methods 0.000 description 2
- 229910052799 carbon Inorganic materials 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 238000007598 dipping method Methods 0.000 description 2
- 239000000446 fuel Substances 0.000 description 2
- 238000010191 image analysis Methods 0.000 description 2
- 229910052750 molybdenum Inorganic materials 0.000 description 2
- 238000000465 moulding Methods 0.000 description 2
- 150000004767 nitrides Chemical class 0.000 description 2
- 238000005498 polishing Methods 0.000 description 2
- 238000001556 precipitation Methods 0.000 description 2
- 239000006104 solid solution Substances 0.000 description 2
- 239000000126 substance Substances 0.000 description 2
- 230000000007 visual effect Effects 0.000 description 2
- 229910001335 Galvanized steel Inorganic materials 0.000 description 1
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 description 1
- 238000004364 calculation method Methods 0.000 description 1
- 229910002092 carbon dioxide Inorganic materials 0.000 description 1
- 239000001569 carbon dioxide Substances 0.000 description 1
- 238000009749 continuous casting Methods 0.000 description 1
- 238000007796 conventional method Methods 0.000 description 1
- 239000013078 crystal Substances 0.000 description 1
- 238000009792 diffusion process Methods 0.000 description 1
- 238000009713 electroplating Methods 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 238000011156 evaluation Methods 0.000 description 1
- 230000008014 freezing Effects 0.000 description 1
- 238000007710 freezing Methods 0.000 description 1
- 239000008397 galvanized steel Substances 0.000 description 1
- 230000001771 impaired effect Effects 0.000 description 1
- 230000003993 interaction Effects 0.000 description 1
- 229910052748 manganese Inorganic materials 0.000 description 1
- 238000000691 measurement method Methods 0.000 description 1
- 229910052698 phosphorus Inorganic materials 0.000 description 1
- 238000003825 pressing Methods 0.000 description 1
- 238000007670 refining Methods 0.000 description 1
- 229920006395 saturated elastomer Polymers 0.000 description 1
- 238000001878 scanning electron micrograph Methods 0.000 description 1
- 229910052710 silicon Inorganic materials 0.000 description 1
- 239000007858 starting material Substances 0.000 description 1
- 238000009864 tensile test Methods 0.000 description 1
Images
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/005—Ferrous alloys, e.g. steel alloys containing rare earths, i.e. Sc, Y, Lanthanides
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
- C21D8/0205—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips of ferrous alloys
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- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
- C21D8/0221—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the working steps
- C21D8/0226—Hot rolling
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- 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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- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
- C21D8/0247—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the heat treatment
- C21D8/0273—Final recrystallisation annealing
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- 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
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- 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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- C22C38/008—Ferrous alloys, e.g. steel alloys containing tin
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- 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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- 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
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- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/08—Ferrous alloys, e.g. steel alloys containing nickel
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- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/10—Ferrous alloys, e.g. steel alloys containing cobalt
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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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- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/14—Ferrous alloys, e.g. steel alloys containing titanium or zirconium
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- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/16—Ferrous alloys, e.g. steel alloys containing copper
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- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
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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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- 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
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- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/32—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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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/60—Ferrous alloys, e.g. steel alloys containing lead, selenium, tellurium, or antimony, or more than 0.04% by weight of sulfur
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- 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
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- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D2211/00—Microstructure comprising significant phases
- C21D2211/002—Bainite
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- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D2211/00—Microstructure comprising significant phases
- C21D2211/005—Ferrite
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- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D2211/00—Microstructure comprising significant phases
- C21D2211/008—Martensite
Definitions
- the present invention mainly relates to a high-strength steel sheet used as an automobile part and a method for manufacturing the same. Specifically, the present invention relates to a high-strength steel sheet having a yield strength of 550 MPa or more and excellent in material uniformity in the width direction, and a method for producing the same.
- Patent Document 1 discloses a high-strength cold-rolled steel sheet having a steel plate shape and shape freezing property of 980 MPa or more and a method for producing the same.
- Patent Document 2 discloses a high-strength cold-rolled steel sheet excellent in elongation and stretch flangeability and a manufacturing method thereof.
- Patent Document 3 discloses a high-strength hot-dip galvanized steel sheet excellent in formability and impact resistance and a method for producing the same.
- the present invention advantageously solves the above-described problems of the prior art, and provides a high-strength steel sheet having a yield strength of 550 MPa or more having a small amount of springback and uniform material in the width direction, and a method for producing the same. With the goal.
- the present inventors have made extensive studies on the microstructure of steel, and as a result, have obtained the following knowledge.
- (1) The material variation in the width direction is easily affected by the microstructure that can be observed from the plate thickness section in the direction perpendicular to the rolling direction.
- (2) Material variation in the width direction tends to occur due to temperature unevenness such as the temperature used for adjusting the annealing temperature and the cooling rate.
- the above material variation Can be suppressed.
- the martensite phase and the ferrite phase become coarse, a hard portion and a soft portion are locally generated, and the material variation in the width direction tends to increase.
- the present invention has been completed based on the above findings. More specifically, the present invention provides the following.
- the component composition further includes, by mass%, Cu, Ni, Sn, As, Sb, Ca, Mg, Pb, Co, Ta, W, REM, Zn, Sr, Cs, Hf, V, and Nb.
- the high-strength steel sheet of the present invention has a yield strength of 550 MPa or more and excellent uniformity in the material in the width direction.
- C 0.05 to 0.15% C is an element necessary for generating a martensite phase and increasing the strength. If the C content is less than 0.05%, the hardness of the martensite phase decreases and the yield strength does not become 550 MPa or more. On the other hand, if the C content exceeds 0.15%, ductility deteriorates due to the generation of a large amount of cementite. In addition, material variation in the width direction increases. Therefore, the C content is 0.05 to 0.15%.
- the lower limit is preferably 0.06% or more. More preferably, it is 0.07% or more, More preferably, it is 0.08% or more.
- the upper limit is preferably 0.14% or less, more preferably 0.12% or less, and still more preferably 0.10% or less.
- Si 0.010 to 2.0% Si is an element having an effect of increasing the hardness of the steel sheet by solid solution strengthening. In order to ensure the yield strength stably, the Si content is set to 0.010% or more. On the other hand, when the Si content exceeds 2.0%, cementite is finely precipitated in the martensite phase and the ductility deteriorates. In addition, material variation in the width direction increases. Therefore, the Si content is set to 2.0% or less.
- the lower limit is preferably 0.3% or more. More preferably, it is 0.5% or more, More preferably, it is 0.7% or more.
- the upper limit is preferably 1.80% or less. More preferably, it is 1.70% or less, More preferably, it is 1.60% or less.
- Mn 1.8-3.2%
- Mn is an element having an effect of increasing the hardness of the steel sheet by solid solution strengthening.
- Mn is an element that suppresses ferrite transformation and generates a martensite phase to increase the strength of the material.
- the Mn content needs to be 1.8% or more.
- it is 2.0% or more. More preferably, it is 2.1% or more, More preferably, it is 2.2% or more.
- the Mn content is set to 3.2% or less.
- it is 3.0% or less. More preferably, it is 2.8% or less, and further preferably 2.7% or less.
- the P content is 0.05% or less. Preferably it is 0.03% or less, More preferably, it is 0.02% or less. Moreover, the lower limit of the P content is not particularly limited, but 0.0001% or more is preferable from the viewpoint of manufacturing cost.
- S 0.02% or less S combines with Mn to form coarse MnS and lowers ductility. For this reason, it is preferable to reduce S content as much as possible.
- the S content may be 0.02% or less. Preferably it is 0.01% or less, More preferably, it is 0.002% or less.
- the lower limit of the S content is not particularly limited, but is preferably 0.0001% or more from the viewpoint of manufacturing cost.
- Al 0.01 to 2.0% Deoxidation is important because the ductility decreases when a large amount of oxide is present in the steel. Moreover, Al may suppress the precipitation of cementite. In order to obtain these effects, the Al content needs to be 0.01% or more. On the other hand, if the Al content exceeds 2.0%, the oxides and nitrides are coarsened and the ductility is lowered. Therefore, the Al content is set to 2.0% or less.
- the lower limit is preferably 0.02% or more. More preferably, it is 0.03% or more, More preferably, it is 0.05% or more.
- the upper limit is preferably 1.5% or less. More preferably, it is 0.1% or less.
- Mo is an important element for suppressing the material variation in the width direction. Mo promotes nucleation of austenite and refines martensite. Further, ferrite is refined by grain boundary segregation of Mo. In order to obtain this effect, the Mo content needs to be 0.03% or more. Preferably it is 0.05% or more. More preferably, it is 0.07% or more, More preferably, it is 0.10% or more. On the other hand, when the Mo content exceeds 0.50%, since the interaction between Mo and C is strong, the diffusion of C in the austenite is suppressed, and the bainite transformation is suppressed. Further, the carbide is precipitated and the ductility is deteriorated. Preferably it is 0.40% or less, More preferably, it is 0.35% or less, More preferably, it is 0.30% or less.
- B 0.0001 to 0.005%
- B is an element useful for suppressing the formation of a pearlite phase from the austenite phase and ensuring a desired martensite fraction (martensite area ratio).
- the B content needs to be 0.0001% or more.
- it is 0.0010% or more, More preferably, it is 0.0015% or more.
- the B content is set to 0.005% or less.
- it is 0.004% or less, More preferably, it is 0.003% or less, More preferably, it is 0.0020% or less.
- Ti 0.005 to 0.04% Ti combines with N to form nitrides, thereby suppressing the formation of BN, drawing out the effect of B, and forming TiN to refine crystal grains and improve toughness.
- the Ti content needs to be 0.005% or more. Preferably it is 0.01% or more.
- Ti content exceeds 0.04%, not only this effect is saturated, but also the rolling load is increased, so that stable steel plate production becomes difficult. Therefore, Ti's dormitory is 0.04% or less. Preferably it is 0.03% or less.
- Cr 1.0% or less
- Cr is an element having an effect of suppressing temper embrittlement. Therefore, the effect of the present invention is further increased by adding Cr.
- it is preferable to contain 0.005% or more. More preferably, it is 0.010% or more.
- the Cr content is 1.0% or less.
- it is 0.5% or less. More preferably, it is 0.2% or less.
- the high-strength steel sheet of the present invention is any one of Cu, Ni, Sn, As, Sb, Ca, Mg, Pb, Co, Ta, W, REM, Zn, Sr, Cs, Hf, V, and Nb.
- the lower limit is not particularly limited, but the total is preferably 0.001% or more.
- Components other than the above are Fe and inevitable impurities.
- the effect of this invention is not impaired. Therefore, when the above arbitrary element is included below the lower limit value, it is assumed that the arbitrary element is included as an inevitable impurity.
- the microstructure of the high-strength steel sheet of the present invention is a structure specified by observing a sheet thickness section that appears when the steel sheet is cut in the sheet width direction (perpendicular to the rolling direction). Specifically, it has the following characteristics.
- the microstructure of the high-strength steel sheet of the present invention contains the bainite phase in an area ratio of 5 to 30%. Since the bainite phase is generated from the austenite grain boundary, the formation of the bainite phase is effective in refining the martensite phase. In addition, the strength of the bainite phase is intermediate between martensite and ferrite, and has an effect of suppressing the material variation due to workability and hardness. In order to sufficiently obtain this effect, the area fraction (area ratio) of the bainite phase needs to be 5% or more. Preferably it is 9% or more. More preferably, it is 11% or more.
- the area ratio of the bainite phase is set to 30% or less. Preferably it is 25% or less, more preferably 20% or less.
- the microstructure of the high-strength steel sheet of the present invention contains the martensite phase in an area ratio of 40 to 70%.
- the martensite phase is a hard phase and has an effect of increasing the strength of the steel sheet by strengthening the transformation structure.
- the area fraction (area ratio) of the martensite phase needs to be 40% or more. Preferably it is 45% or more, more preferably 50% or more.
- the area ratio of the martensite phase exceeds 70%, the hard phase is locally coarsened and the uniformity of the material is lowered. Therefore, the area ratio of the martensite phase is 70% or less.
- the martensite phase includes both a tempered martensite phase and an as-quenched martensite phase.
- the total of bainite and martensite phase is preferably 55% or more.
- the average particle size of the martensite phase is 2 to 8 ⁇ m. In order to make the yield strength 550 MPa or more, it is necessary to make the average particle size of the martensite phase 2 ⁇ m or more. Preferably it is 4 micrometers or more, More preferably, it is 5 micrometers or more. On the other hand, when the average particle size of the martensite phase exceeds 8 ⁇ m, the hard phase is locally coarsened and the uniformity of the material is lowered. Therefore, the average particle size of the martensite phase is 8 ⁇ m or less. Preferably, it is 7 ⁇ m or less.
- the area ratio of the ferrite phase is not particularly limited, but is preferably 5 to 40%. 5% or more is preferable because the ferrite phase is excellent in workability. More preferably, it is 11% or more, More preferably, it is 15% or more. If the area ratio of the ferrite phase exceeds 40%, the yield strength may be 550 MPa or less. More preferably, it is 35% or less.
- the average particle diameter of the ferrite phase contained in the microstructure is 11 ⁇ m or less.
- the average particle diameter of the ferrite phase exceeds 11 ⁇ m, the strength of the steel sheet is lowered and the toughness is deteriorated.
- the soft phase is locally coarsened and the material uniformity is reduced. Therefore, the average particle diameter of the ferrite phase is set to 11 ⁇ m or less.
- the preferable average particle diameter for the lower limit is 3 ⁇ m or more. More preferably, it is 4 micrometers or more, More preferably, it is 5 micrometers or more.
- the preferable average particle diameter for the upper limit is 10 ⁇ m or less. More preferably, it is 9 micrometers or less, More preferably, it is 8 micrometers or less.
- the average particle diameter of a ferrite phase shall be 3.0 times or less of the average particle diameter of a martensite. Preferably it is 2.5 times or less, More preferably, it is 2.0 times or less. The lower limit is preferably 1.0 times or more. More preferably, it is 1.2 times or more.
- the microstructure includes bainite, martensite phase, and ferrite phase, but may include phases other than these.
- Other phases include pearlite, retained austenite, and the like.
- the total area ratio of the other phases is preferably 8% or less.
- the average grain size of the martensite phase and the average grain size of the ferrite phase are the thickness 1 / of the thickness section (C section) that appears when the steel sheet is cut in a direction perpendicular to the rolling direction (perpendicular direction). Measure by observing 4 parts. Specifically, the corrosion appearing structure with 1% nital is magnified 2000 times with a scanning electron microscope (SEM), taken for 10 fields of view, and determined by a cutting method in accordance with ASTM E 112-10.
- the ferrite phase is a structure having a form in which corrosion marks and cementite are not observed in the grains, and the bainite phase is a structure in which corrosion marks and large carbides are recognized in the grains.
- Martensite that has not been tempered has no cementite in the grains and has a brighter contrast than the ferrite phase, and tempered martensite has a structure in which corrosion marks and cementite are recognized in the grains.
- the average of the area ratio with respect to an observation visual field was calculated
- cold rolled steel sheet or hot-dip steel sheet steel sheet is ground to 1/4 position with respect to the thickness direction, and chemical polishing of 200 ⁇ m or more is performed.
- the volume fraction of the retained austenite phase was quantified by the X-ray diffraction intensity of the applied plate surface.
- the incident radiation source was MoK ⁇ radiation and measured from the peaks of (200) ⁇ , (211) ⁇ , (220) ⁇ , (200) ⁇ , (220) ⁇ , (311) ⁇ .
- the volume ratio value of the obtained retained austenite phase was the value of the area ratio of the steel sheet structure.
- the martensite area ratio of the present invention was a value obtained by reducing the area ratio of retained austenite from the tempered martensite area ratio and adding the area ratio of tempered martensite. Moreover, the area ratio of each phase can also be calculated
- the high-strength steel sheet having the above component composition and microstructure may have a plating layer on the surface.
- the type of the plating layer is not particularly limited, but a hot dip galvanizing layer is preferable. Further, an alloyed hot dip galvanized layer formed by alloying is also preferable.
- the manufacturing method of the high strength steel sheet of the present invention may use a cold rolled steel sheet as a starting material.
- a cold rolled steel sheet as a starting material.
- the method for producing a high-strength steel sheet described below includes a hot rolling process, a cold rolling process, an annealing process, and a plating process.
- the melting method of the steel material is not particularly limited, and a known melting method such as a converter or an electric furnace can be employed. Moreover, after melting, it is preferable to use a slab (steel material) by continuous casting because of problems such as segregation.
- the slab may be formed by a known casting method such as ingot-bundling rolling or continuous slab casting.
- the slab may be re-heated in a heating furnace and then rolled. May be.
- Hot rolling step The steel material obtained above is subjected to rough rolling and finish rolling.
- it is necessary to dissolve carbides in the steel material before rough rolling.
- the heating temperature of the slab is preferably 1300 ° C. or lower.
- the process of heating the steel material before rough rolling is It can be omitted.
- the rough rolling conditions are not particularly limited.
- Cold rolling process In the cold rolling process, the hot rolled steel sheet obtained in the hot rolling process is cold-rolled.
- the rolling rate in cold rolling is not particularly limited, and may be set as appropriate.
- a cold-rolled steel sheet having the above component composition (a cold-rolled steel sheet obtained by using a steel material having the above-mentioned component composition) is subjected to average heating in a temperature range of A c1 -50 ° C. to A c1. Heat to the annealing temperature at a speed of 10 ° C./s or higher.
- a c1 ferrite ⁇ austenite transformation start temperature
- the average heating rate at A c1 -50 ° C. to A c1 is less than 10 ° C./s, the nucleation of the austenite phase is small, and the particle size becomes coarse in the martensite phase of the final structure.
- an upper limit is not specifically limited, 30 degrees C / s or less is preferable.
- Ac1 can be calculated
- the element symbol means the content (% by mass) of each element, and 0 is not included.
- a c1 (° C.) 723 + 29.1Si-10.7Mn-16.9Ni + 16.9Cr
- annealing is performed under conditions of annealing temperature: 750 to 900 ° C.
- the martensite phase is contained in a volume fraction of 40 to 70%, and the average particle size of the ferrite phase is 11 ⁇ m or less. It is necessary to anneal the hot-rolled steel sheet by holding it at an annealing temperature of 750 to 900 ° C. for 30 to 200 seconds. When the annealing temperature is less than 750 ° C. or the holding time is less than 30 s, the ferrite fraction increases and the final structure does not contain the desired amount of bainite and martensite phase.
- the annealing temperature exceeds 900 ° C.
- the volume fraction of martensite increases and the uniformity of the material decreases.
- annealing time exceeds 200 second, ductility may be reduced by precipitation of a large amount of iron carbide.
- material variation in the width direction increases. Therefore, the annealing temperature is 750 to 900 ° C., and the annealing time is 30 to 200 seconds.
- a preferable annealing temperature for the lower limit is 800 ° C. or higher.
- a preferable annealing temperature for the upper limit is 900 ° C. or less.
- a preferable annealing time for the lower limit is 50 seconds or more.
- the preferable annealing time for the upper limit is 150 seconds or less.
- the cooling rate is 10 to 40 ° C./s.
- it shall be 30 degrees C / s or less.
- bending and unbending is performed 2 to 6 times in total with a roll having a radius of 100 mm or more.
- a roll having a radius of 100 mm or more In order to make the average particle size of the martensite phase 2-8 ⁇ m and the average particle size of the ferrite phase 11 ⁇ m or less, it is necessary to suppress grain growth during cooling after annealing. This process is effective for suppressing material fluctuation in the width direction. Therefore, it is necessary to bend and unbend twice to six times during the cooling. Bending and bending back using a roll having a radius of less than 100 mm and bending and bending back less than twice do not provide the desired particle size. Moreover, material fluctuation cannot be suppressed sufficiently.
- the roll diameter was set to 100 mm or more and the number of times of bending and bending was set to 2 times or more.
- the martensite phase tends to be hardened and the uniformity of the material is lowered. Therefore, it was set to bend and bend back 6 times or less. Preferably it is 4 times or less.
- the sum total of the number of times of bending and bending back means two times or more.
- the thickness at the time of bending and bending back is not particularly limited, but is usually 0.5 to 2.6 mm.
- a plating step for performing the following plating treatment may be performed.
- the type of plating treatment is not particularly limited, and any of electroplating treatment and hot dipping treatment may be used.
- An alloying process may be performed after the hot dipping process. Preferably, it is a hot dip galvanizing treatment or an alloying hot dip galvanizing treatment in which an alloying treatment is performed after the hot dip galvanizing treatment.
- the plating process may be performed after the cooling is stopped at 400 to 600 ° C., the cooling process may be further performed, and then the plating process may be performed.
- a steel sheet having a thickness of 1.2 mm was manufactured by subjecting the slab having the composition shown in Table 1 to hot rolling, cold rolling and annealing under the conditions shown in Table 2.
- Table 1 A steel sheet having the composition shown in Table 1 to hot rolling, cold rolling and annealing under the conditions shown in Table 2.
- a sample was taken from a position 50 mm from the center and end in the width direction, and the change in characteristics was investigated. Evaluation was based on the absolute value of the material difference between the center and the end in the width direction.
- the survey method is as follows.
- vertical to the rolling direction of the obtained steel plate was grind
- the image is magnified 2000 times with a scanning electron microscope, 10 areas of the area from the surface to a thickness of 1/4 t are imaged and determined by a cutting method in accordance with ASTM E 112-10.
- t is the thickness (plate thickness) of the steel plate. Based on the captured image, the area ratio of each phase was measured.
- the ferrite phase is a structure having a form in which corrosion marks and cementite are not observed in the grains
- the bainite phase is a structure in which corrosion marks and large carbides are recognized in the grains.
- Martensite that has not been tempered has no cementite in the grains and has a brighter contrast than the ferrite phase, and tempered martensite has a structure in which corrosion marks and cementite are recognized in the grains.
- the average of the area ratio with respect to an observation visual field was calculated
- the retained austenite is measured by the X-ray diffraction intensity of the plate surface that is ground to 1 ⁇ 4 position in the thickness direction and subjected to chemical polishing for 200 ⁇ m or more. The volume fraction of the phase was quantified.
- the incident radiation source was MoK ⁇ radiation and measured from the peaks of (200) ⁇ , (211) ⁇ , (220) ⁇ , (200) ⁇ , (220) ⁇ , (311) ⁇ .
- the volume ratio value of the obtained retained austenite phase was the value of the area ratio of the steel sheet structure.
- the martensite area ratio of the present invention was regarded as a value obtained by reducing the area ratio of retained austenite from the martensite area ratio not tempered and adding the area ratio of tempered martensite. In addition, pearlite was confirmed as another phase.
- the martensite average particle diameter and the ferrite average particle diameter were magnified 1000 times with a scanning electron microscope (SEM) and photographed for 10 fields of view. It was determined by a cutting method in accordance with ASTM E 112-10. Table 3 shows the calculated average particle diameter of martensite and the average particle diameter of ferrite.
- TS is preferably 980 MPa or more.
- El is preferably 16% or more.
- Table 3 also shows the difference between the center and end in the width direction. ⁇ YP is 15 MPa or less, ⁇ TS is 20 MPa or less, and ⁇ El is 3.0% or less.
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Abstract
Description
(1)幅方向の材質変動は、圧延直角方向の板厚断面から観察できるミクロ組織の影響を受けやすい。
(2)幅方向の材質変動は、焼鈍温度や冷却速度の調整に用いる温度などの温度ムラにより生じる傾向にある。特定の成分組成及び特定の製造方法を採用して、圧延方向に対して直角方向に鋼板を切断したときに現れる板厚断面のミクロ組織を、特定のミクロ組織とすることで、上記材質変動を抑制できる。
(3)マルテンサイト相及びフェライト相が粗大化すると、局部的に硬質部分と軟質部分が発生し、幅方向の材質変動が大きくなる傾向にある。
Cは、マルテンサイト相を生成させて強度を上昇させるために必要な元素である。C含有量が0.05%未満では、マルテンサイト相の硬さが低下し、降伏強さが550MPa以上にならない。一方、C含有量が0.15%を超えるとセメンタイトが多量に生成するころにより延性が劣化する。また、幅方向の材質変動が大きくなる。したがって、C含有量は0.05~0.15%とする。下限について好ましくは0.06%以上である。より好ましくは0.07%以上、さらに好ましくは0.08%以上である。上限について好ましくは0.14%以下、より好ましくは0.12%以下、さらに好ましくは0.10%以下とする。
Siは固溶強化により鋼板の硬度を高める作用を有する元素である。降伏強さを安定的に確保するために、Si含有量を0.010%以上とする。一方、Si含有量が2.0%を超えると、セメンタイトが微細にマルテンサイト相中に析出して、延性が劣化する。また、幅方向の材質変動が大きくなる。そこで、Si含有量は2.0%以下とする。下限について好ましくは0.3%以上である。より好ましくは0.5%以上、さらに好ましくは0.7%以上である。上限について好ましくは1.80%以下である。より好ましくは1.70%以下、さらに好ましくは1.60%以下である。
Mnは固溶強化により鋼板の硬度を高める作用を有する元素である。また、Mnはフェライト変態を抑えてマルテンサイト相を生成させて素材の強度を上昇させる元素である。降伏強さを安定的に確保するため、Mn含有量は1.8%以上の含有を必要とする。好ましくは2.0%以上である。より好ましくは2.1%以上、さらに好ましくは2.2%以上である。一方、Mn含有量が多くなると、偏析層により成形性が低下したり、幅方向の材質変動が大きくなったりするので、Mn含有量は3.2%以下とする。好ましくは3.0%以下である。より好ましくは2.8%以下、さらに好ましくは2.7%以下である。
Pは粒界に偏析して延性を低下させる。そのため、P含有量は0.05%以下とする。好ましくは0.03%以下であり、さらに好ましくは0.02%以下である。また、P含有量の下限は特に限定されないが、製造コストの観点からは0.0001%以上が好ましい。
Sは、Mnと結合して粗大なMnSを形成し、延性を低下させる。このため、S含有量はできるだけ低減することが好ましい。本発明では、S含有量は0.02%以下であればよい。好ましくは0.01%以下であり、さらに好ましくは0.002%以下である。また、S含有量の下限は特に限定されないが、製造コストの観点からは0.0001%以上が好ましい。
鋼中に酸化物が大量に存在すると延性が低下することから脱酸は重要である。また、Alはセメンタイトの析出を抑制することがある。これらの効果を得るために、Al含有量は0.01%以上とする必要がある。一方、Al含有量が2.0%を超えると、酸化物や窒化物が凝集粗大化して延性が低下する。そこで、Al含有量は2.0%以下とした。下限について好ましくは0.02%以上である。より好ましくは0.03%以上、さらに好ましくは0.05%以上である。上限について好ましくは1.5%以下である。より好ましくは0.1%以下である。
Moは、本発明において、幅方向の材質変動を抑えるために重要な元素である。Moはオーステナイトの核生成を促進し、マルテンサイトを微細化させる。またMoの粒界偏析によりフェライトを微細化させる。この効果を得るために、Moの含有量は0.03%以上にする必要がある。好ましくは0.05%以上である。より好ましくは0.07%以上、さらに好ましくは0.10%以上である。一方、Mo含有量が0.50%を超えると、MoとCの相互作用が強いため、オーステナイト中のCの拡散を抑制し、ベイナイト変態を抑制する。また炭化物が析出して延性が劣化してしまう。好ましくは0.40%以下、さより好ましくは0.35%以下、さらに好ましくは、0.30%以下である。
Bはオーステナイト相からのパーライト相の生成を抑制し、所望のマルテンサイト分率(マルテンサイトの面積率)を確保するために役立つ元素である。この効果を十分に得るには、Bの含有量は0.0001%以上にする必要がある。好ましくは0.0010%以上、より好ましくは0.0015%以上である。一方、B含有量が0.005%を超えると、BはFe23(CB)6を形成して延性を劣化させる。そこで、B含有量を0.005%以下とする。好ましくは0.004%以下、より好ましくは、0.003%以下、さらに好ましくは0.0020%以下である。
TiはNと結合し、窒化物を形成することにより、BNの形成を抑制し、Bの効果を引き出すとともに、TiNを形成させて結晶粒を微細化して靱性を向上させる。この効果を十分に得るためには、Ti含有量を0.005%以上にする必要がある。好ましくは0.01%以上である。一方、Ti含有量が0.04%を超えると、この効果が飽和するだけではなく、圧延負荷を高めるため、安定した鋼板製造が困難になる。そこで、Tiが入寮は0.04%以下とする。好ましくは0.03%以下である。
Crは焼き戻し脆化を抑制する効果を持つ元素である。そのため、Crを添加することで本発明の効果はさらに増大する。この効果を得るためには0.005%以上含有することが好ましい。より好ましくは0.010%以上である。しかしながら、Cr含有量が1.0%を超えると、Cr炭化物が形成され、延性が劣化する。そこで、Crを含む場合、Cr含有量は1.0%以下とする。好ましくは0.5%以下である。より好ましくは0.2%以下である。
本発明の高強度鋼板のミクロ組織は、ベイナイト相を面積率で5~30%含む。ベイナイト相は、オーステナイト粒界から生成するため、ベイナイト相の生成によりマルテンサイト相の微細化に効果がある。またベイナイト相の強度はマルテンサイト及びフェライトの中間であり、加工性及び硬度さによる材質の変動を抑制する作用を有している。この効果を十分に得るためには、ベイナイト相の面積分率(面積率)は5%以上にする必要がある。好ましくは9%以上である。より好ましくは11%以上である。一方、ベイナイト相の面積率が30%を超えると、マルテンサイト分率が低下し、降伏強度を550MPa以上得られなくなる。そこで、ベイナイト相の面積率を30%以下とする。好ましくは25%以下、より好ましくは20%以下である。
本発明の高強度鋼板のミクロ組織は、マルテンサイト相を面積率で40~70%含む。マルテンサイト相は、硬質相であり、変態組織強化によって鋼板の強度を増加させる作用を有している。また、降伏強さを550MPa以上にするには、マルテンサイト相の面積分率(面積率)は40%以上にする必要がある。好ましくは45%以上、より好ましくは50%以上である。一方、マルテンサイト相の面積率が70%を超えると、局部的に硬質相が粗大化し、材質の均一性が低下する。そこで、マルテンサイト相の面積率は70%以下とする。好ましくは65%以下、より好ましくは60%以下である。また、マルテンサイト相とは、焼戻しマルテンサイト相、焼入れままマルテンサイト相の両方を含む。なお、ベイナイトとマルテンサイト相の合計は55%以上が好ましい。
フェライト相の平均粒径とマルテンサイトの平均粒径の差が大きくなると、局部的に硬質相や軟質相が粗大化し、材質の均一性が低下し、幅方向の材質変動が大きくなる。このため、フェライト相の平均粒径がマルテンサイトの平均粒径の3.0倍以下とする。好ましくは2.5倍以下、より好ましくは2.0倍以下である。下限については1.0倍以上が好ましい。より好ましくは1.2倍以上である。
ここで、マルテンサイト相の平均粒径、フェライト相の平均粒径は、圧延方向に垂直方向(直角方向)に鋼板を切断したときに現れる板厚断面(C断面)の板厚1/4部を観察することで測定する。具体的には、1%ナイタールによる腐食現出組織を走査型電子顕微鏡(SEM)で2000倍に拡大して、10視野分撮影し、ASTM E 112-10に準拠した切断法によって求める。フェライト相は粒内に腐食痕やセメンタイトが観察されない形態を有する組織であり、ベイナイト相は粒内に腐食痕や大きな炭化物が認められる組織である。焼き戻しされていないマルテンサイトは粒内にセメンタイトが認められず、フェライト相よりも明るいコントラストであり、焼き戻しマルテンサイトは粒内に腐食痕やセメンタイトが認められる組織である。これらの相について画像解析により観察視野に対する面積率の平均を求めた。また、マルテンサイトと残留オーステナイトを区別するため、残留オーステナイトの測定について、冷延鋼板もしくは溶融めっき鋼板の地鉄鋼板を板厚方向に対して1/4位置まで研削加工し、200μm以上化学研磨を施した板面のX線回折強度により残留オーステナイト相の体積率を定量した。入射線源はMoKα線を用い、(200)α、(211)α、(220)α、(200)γ、(220)γ、(311)γのピークから測定した。得られた残留オーステナイト相の体積率の値は鋼板組織の面積率の値とした。本発明のマルテンサイト面積率は焼き戻しされていないマルテンサイト面積率から残留オーステナイトの面積率を減らし、焼き戻しマルテンサイトの面積率を足した値とした。また、各相の面積率も上記SEM画像から求めることができる。
上記の得られた鋼素材に、粗圧延および仕上げ圧延を施すが、本発明においては、粗圧延前に鋼素材中の炭化物を溶解する必要がある。スラブを加熱する場合は、炭化物を溶解させたり、圧延荷重の増大を防止したりするため、1100℃以上に加熱することが好ましい。また、スケールロスの増大を防止するため、スラブの加熱温度は1300℃以下とすることが好ましい。また、先述のとおり、粗圧延前の鋼素材が、所定温度以上の温度を保持しており、鋼素材中の炭化物が溶解している場合には、粗圧延前の鋼素材を加熱する処理は省略可能である。なお、粗圧延条件については特に限定する必要はない。
冷延工程では、熱延工程で得られた熱延鋼板を冷間圧延する。冷間圧延における圧延率は特に限定されず、適宜設定すればよい。
焼鈍工程では、先ず、上記成分組成を有する冷延鋼板(上記成分組成を有する鋼素材を用いることで得られる冷延鋼板)を、Ac1-50℃~Ac1の温度域の平均加熱速度が10℃/s以上の条件で焼鈍温度まで加熱する。マルテンサイト相を微細化にするには、オーステナイト相の核生成を促進する必要がある。オーステナイト相の核生成を促進するには、Ac1点(フェライト→オーステナイト変態開始温度)-50℃~Ac1の平均加熱速度を速くする必要がある。Ac1-50℃~Ac1での平均加熱速度が10℃/s未満になると、オーステナイト相の核生成が少なく、最終組織のマルテンサイト相に粒径が粗大化になる。上限は特に限定されないが、30℃/s以下が好ましい。なお、Ac1は下記の式を用いて求めることができる。下記式において元素記号は各元素の含有量(質量%)を意味し、含まないものは0とする。
Ac1(℃)=723+29.1Si-10.7Mn-16.9Ni+16.9Cr
次いで、焼鈍温度:750~900℃、焼鈍時間:30~200秒の条件で焼鈍する。マルテンサイト相の平均粒径が2~8μmであり、体積分率で40~70%のマルテンサイト相を含有し、且つフェライト相の平均粒径が11μm以下であるミクロ組織とするには、冷間圧延後の鋼板を750~900℃の焼鈍温度で30~200秒保持して焼鈍する必要がある。焼鈍温度が750℃未満や保持時間が30s未満の場合、フェライト分率が大きくなり、最終組織に所望量のベイナイト及びマルテンサイト相が含まれない。一方、焼鈍温度が900℃を超えると、マルテンサイトの体積分率が高くなり、材質の均一性が低下する。また、焼鈍時間が200秒を超えると、鉄炭化物の多量の析出により延性の低下を招くことがある。また、幅方向の材質変動が大きくなる。したがって、焼鈍温度は750~900℃、焼鈍時間は30~200秒とする。また、下限について好ましい焼鈍温度は800℃以上である。上限について好ましい焼鈍温度は900℃以下である。下限について好ましい焼鈍時間は50秒以上とする。上限について好ましい焼鈍時間は150秒以下とする。
得られた鋼板の圧延方向に垂直な板厚断面を研磨して、1%ナイタールによる腐食現出させた。走査型電子顕微鏡で2000倍に拡大して、表面から板厚1/4t部までの領域内を10視野分撮影し、ASTM E 112-10に準拠した切断法によって求める。tは鋼板の厚さ(板厚)である。上記撮影画像に基づき、各相の面積率を測定した。フェライト相は粒内に腐食痕やセメンタイトが観察されない形態を有する組織であり、ベイナイト相は粒内に腐食痕や大きな炭化物が認められる組織である。焼き戻しされていないマルテンサイトは粒内にセメンタイトが認められず、フェライト相よりも明るいコントラストであり、焼き戻しマルテンサイトは粒内に腐食痕やセメンタイトが認められる組織である。これらの相について画像解析により観察視野に対する面積率の平均を求めた。また、マルテンサイトと残留オーステナイトを区別するため、残留オーステナイトの測定について、板厚方向に対して1/4位置まで研削加工し、200μm以上化学研磨を施した板面のX線回折強度により残留オーステナイト相の体積率を定量した。入射線源はMoKα線を用い、(200)α、(211)α、(220)α、(200)γ、(220)γ、(311)γのピークから測定した。得られた残留オーステナイト相の体積率の値は鋼板組織の面積率の値とした。本発明のマルテンサイト面積率は焼き戻しされていないマルテンサイト面積率から残留オーステナイトの面積率を減らして、焼き戻しマルテンサイトの面積率を足した値とみなした。なお、その他の相としてパーライトが確認された。
圧延方向と90°の方向を長手方向(引張方向)とするJIS Z 2201に記載の5号試験片を用い、JIS Z 2241に準拠した引張試験を5回行い、平均の降伏強さ(YP)、引張強さ(TS)、突合せ伸び(EL)を求めた。算出結果を表3に示す。YPは550MPa以上を良好とする。
圧延方向に平行する方向を長手方向とした幅35mm、長さ100mmの鋼板を切り出し、試験片を作製した。作製した試験片を図1のように押金具で成形荷重10kN、荷重速度100mm/min、曲げ半径R=4mmでL曲げ試験を行った。図2のθ値をスプリングパック角度とした。これらの結果を表3にまとめて示す。θは9.0°以下を良好とする。幅方向の中央部と端部との差についても表3に示した。Δθが2.5°以下を良好とする。
Claims (9)
- 質量%で、
C:0.05~0.15%、
Si:0.010~2.0%、
Mn:1.8~3.2%、
P:0.05%以下、
S:0.02%以下、
Al:0.01~2.0%、
Mo:0.03~0.50%を含有し、残部が鉄および不可避的不純物からなる成分組成と、
フェライト相と、面積率で40~70%のマルテンサイト相と、面積率で5~30%のベイナイト相とを含有し、圧延直角方向の板厚断面において、マルテンサイト相の平均粒径が2~8μmであり、フェライト相の平均粒径が11μm以下であり、フェライト相の平均粒径がマルテンサイトの平均粒径の3.0倍以下であるミクロ組織を有し、
降伏強さ(YP)が550MPa以上である高強度鋼板。 - 前記成分組成は、さらに、質量%で、
B:0.0001~0.005%を含有する請求項1に記載の高強度鋼板。 - 前記成分組成は、さらに、質量%で、
Ti:0.005~0.04%を含有する請求項1または請求項2に記載の高強度鋼板。 - 前記成分組成は、さらに、質量%で、
Cr:1.0%以下を含有する請求項1~3のいずれかに記載の高強度鋼板。 - 前記成分組成は、さらに、質量%で、Cu、Ni、Sn、As、Sb、Ca、Mg、Pb、Co、Ta、W、REM、Zn、Sr、Cs、Hf、V、Nbのいずれか1種以上を合計で1%以下含有する請求項1~4のいずれかに記載の高強度鋼板。
- 表面にめっき層を有する請求項1~5のいずれかに記載の高強度鋼板。
- 前記めっき層は、溶融亜鉛めっき層である請求項6に記載の高強度鋼板。
- 請求項1~5のいずれかに記載の成分組成を有する冷延鋼板を、Ac1-50℃~Ac1の温度域の平均加熱速度が10℃/s以上の条件で焼鈍温度まで加熱し、焼鈍温度:750~900℃、焼鈍時間:30~200秒の条件で焼鈍し、10~40℃/sの平均冷却速度で400~600℃まで冷却し、該冷却時に半径100mm以上のロールで曲げ曲げ戻しを合計2回以上6回以下行う焼鈍工程を有する高強度鋼板の製造方法。
- 前記焼鈍工程後、めっき処理を行うめっき工程を有する請求項8に記載の高強度鋼板の製造方法。
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