US20180127856A1 - High-strength cold-rolled steel sheet and method for manufacturing the same - Google Patents
High-strength cold-rolled steel sheet and method for manufacturing the same Download PDFInfo
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- US20180127856A1 US20180127856A1 US15/553,408 US201515553408A US2018127856A1 US 20180127856 A1 US20180127856 A1 US 20180127856A1 US 201515553408 A US201515553408 A US 201515553408A US 2018127856 A1 US2018127856 A1 US 2018127856A1
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- 239000010960 cold rolled steel Substances 0.000 title claims abstract description 167
- 238000000034 method Methods 0.000 title claims abstract description 89
- 238000004519 manufacturing process Methods 0.000 title claims abstract description 21
- 229910001566 austenite Inorganic materials 0.000 claims abstract description 108
- 229910000831 Steel Inorganic materials 0.000 claims abstract description 104
- 239000010959 steel Substances 0.000 claims abstract description 104
- 230000000717 retained effect Effects 0.000 claims abstract description 89
- 229910000734 martensite Inorganic materials 0.000 claims abstract description 78
- 239000013078 crystal Substances 0.000 claims abstract description 59
- 229910000859 α-Fe Inorganic materials 0.000 claims abstract description 48
- 239000000203 mixture Substances 0.000 claims abstract description 21
- 239000000126 substance Substances 0.000 claims abstract description 21
- 239000012535 impurity Substances 0.000 claims abstract description 7
- 229910052748 manganese Inorganic materials 0.000 claims abstract description 6
- 229910052799 carbon Inorganic materials 0.000 claims abstract description 5
- 229910052698 phosphorus Inorganic materials 0.000 claims abstract description 5
- 229910052757 nitrogen Inorganic materials 0.000 claims abstract description 4
- 229910052710 silicon Inorganic materials 0.000 claims abstract description 4
- 229910052717 sulfur Inorganic materials 0.000 claims abstract description 4
- 238000001816 cooling Methods 0.000 claims description 154
- 238000002791 soaking Methods 0.000 claims description 121
- 238000000137 annealing Methods 0.000 claims description 71
- 238000010438 heat treatment Methods 0.000 claims description 69
- 238000005097 cold rolling Methods 0.000 claims description 19
- 238000005098 hot rolling Methods 0.000 claims description 19
- 229910052802 copper Inorganic materials 0.000 claims description 5
- 229910052750 molybdenum Inorganic materials 0.000 claims description 5
- 229910052759 nickel Inorganic materials 0.000 claims description 5
- 229910052758 niobium Inorganic materials 0.000 claims description 2
- 230000008569 process Effects 0.000 description 49
- 229910001563 bainite Inorganic materials 0.000 description 24
- 230000000052 comparative effect Effects 0.000 description 22
- 230000000694 effects Effects 0.000 description 22
- 230000007423 decrease Effects 0.000 description 21
- 229910052729 chemical element Inorganic materials 0.000 description 18
- 230000015572 biosynthetic process Effects 0.000 description 13
- 238000005096 rolling process Methods 0.000 description 11
- 238000005496 tempering Methods 0.000 description 11
- 230000009466 transformation Effects 0.000 description 11
- XEEYBQQBJWHFJM-UHFFFAOYSA-N iron Substances [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 10
- 229910001562 pearlite Inorganic materials 0.000 description 8
- 238000005554 pickling Methods 0.000 description 7
- 229920006395 saturated elastomer Polymers 0.000 description 7
- 150000003568 thioethers Chemical class 0.000 description 6
- 239000000470 constituent Substances 0.000 description 5
- 230000006866 deterioration Effects 0.000 description 5
- 230000002401 inhibitory effect Effects 0.000 description 5
- 238000004080 punching Methods 0.000 description 5
- 229910000794 TRIP steel Inorganic materials 0.000 description 4
- 238000002441 X-ray diffraction Methods 0.000 description 4
- 238000010899 nucleation Methods 0.000 description 4
- 230000006911 nucleation Effects 0.000 description 4
- 238000001953 recrystallisation Methods 0.000 description 4
- 239000006104 solid solution Substances 0.000 description 4
- 238000005728 strengthening Methods 0.000 description 4
- 229910052742 iron Inorganic materials 0.000 description 3
- 150000001247 metal acetylides Chemical class 0.000 description 3
- 230000002441 reversible effect Effects 0.000 description 3
- 238000012360 testing method Methods 0.000 description 3
- 229910001035 Soft ferrite Inorganic materials 0.000 description 2
- 238000005266 casting Methods 0.000 description 2
- 229910001567 cementite Inorganic materials 0.000 description 2
- 230000003247 decreasing effect Effects 0.000 description 2
- 230000007547 defect Effects 0.000 description 2
- 238000005246 galvanizing Methods 0.000 description 2
- KSOKAHYVTMZFBJ-UHFFFAOYSA-N iron;methane Chemical compound C.[Fe].[Fe].[Fe] KSOKAHYVTMZFBJ-UHFFFAOYSA-N 0.000 description 2
- 238000005498 polishing Methods 0.000 description 2
- 238000010791 quenching Methods 0.000 description 2
- 230000000171 quenching effect Effects 0.000 description 2
- 238000005204 segregation Methods 0.000 description 2
- 239000000243 solution Substances 0.000 description 2
- 238000009864 tensile test Methods 0.000 description 2
- 229910052718 tin Inorganic materials 0.000 description 2
- 238000003466 welding Methods 0.000 description 2
- 229910052725 zinc Inorganic materials 0.000 description 2
- 229910000885 Dual-phase steel Inorganic materials 0.000 description 1
- LFQSCWFLJHTTHZ-UHFFFAOYSA-N Ethanol Chemical compound CCO LFQSCWFLJHTTHZ-UHFFFAOYSA-N 0.000 description 1
- 229910001335 Galvanized steel Inorganic materials 0.000 description 1
- -1 MnS are formed Chemical class 0.000 description 1
- GRYLNZFGIOXLOG-UHFFFAOYSA-N Nitric acid Chemical compound O[N+]([O-])=O GRYLNZFGIOXLOG-UHFFFAOYSA-N 0.000 description 1
- 230000001133 acceleration Effects 0.000 description 1
- 229910045601 alloy Inorganic materials 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- 238000005275 alloying Methods 0.000 description 1
- 230000004075 alteration Effects 0.000 description 1
- 229910052787 antimony Inorganic materials 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 238000009749 continuous casting Methods 0.000 description 1
- 238000007796 conventional method Methods 0.000 description 1
- 238000005336 cracking Methods 0.000 description 1
- 239000006185 dispersion Substances 0.000 description 1
- 238000009713 electroplating Methods 0.000 description 1
- 238000005530 etching Methods 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 239000008397 galvanized steel Substances 0.000 description 1
- 238000010191 image analysis Methods 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 229910017604 nitric acid Inorganic materials 0.000 description 1
- 150000004767 nitrides Chemical class 0.000 description 1
- 230000002250 progressing effect Effects 0.000 description 1
- 230000005855 radiation Effects 0.000 description 1
- 238000003303 reheating Methods 0.000 description 1
- 230000002787 reinforcement Effects 0.000 description 1
- 238000009628 steelmaking Methods 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
- 239000013585 weight reducing agent Substances 0.000 description 1
- 229910052726 zirconium Inorganic materials 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
- C21D8/0247—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the heat treatment
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/14—Ferrous alloys, e.g. steel alloys containing titanium or zirconium
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D6/00—Heat treatment of ferrous alloys
- C21D6/005—Heat treatment of ferrous alloys containing Mn
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D6/00—Heat treatment of ferrous alloys
- C21D6/008—Heat treatment of ferrous alloys containing Si
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- 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
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
- C21D8/0247—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the heat treatment
- C21D8/0263—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the heat treatment following hot rolling
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D9/00—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
- C21D9/46—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for sheet metals
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/001—Ferrous alloys, e.g. steel alloys containing N
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/002—Ferrous alloys, e.g. steel alloys containing In, Mg, or other elements not provided for in one single group C22C38/001 - C22C38/60
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/005—Ferrous alloys, e.g. steel alloys containing rare earths, i.e. Sc, Y, Lanthanides
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/02—Ferrous alloys, e.g. steel alloys containing silicon
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/04—Ferrous alloys, e.g. steel alloys containing manganese
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/06—Ferrous alloys, e.g. steel alloys containing aluminium
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/08—Ferrous alloys, e.g. steel alloys containing nickel
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/12—Ferrous alloys, e.g. steel alloys containing tungsten, tantalum, molybdenum, vanadium, or niobium
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/16—Ferrous alloys, e.g. steel alloys containing copper
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
-
- 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
-
- 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
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D2211/00—Microstructure comprising significant phases
- C21D2211/008—Martensite
Definitions
- the present invention relates to a high-strength cold-rolled steel sheet having a high elongation (EL), a high hole expansion ratio ( ⁇ ), and a low yield ratio (YR) and a method for manufacturing the steel sheet, and in particular, to a high-strength cold-rolled steel sheet which can be used for structural parts of, for example, an automobile.
- EL high elongation
- ⁇ high hole expansion ratio
- YR low yield ratio
- examples of known high-strength cold-rolled steel sheet having satisfactory formability and a high strength at the same time include a dual-phase steel sheet (DP steel sheet), which has a multi-phase microstructure composed of ferrite and martensite.
- DP steel sheet has a high elongation (EL)
- a DP steel sheet has a disadvantage in that, since a crack tends to occur due to stress concentration occurring at the interface between ferrite and martensite, there is a deterioration in bendability and hole expansion capability.
- Patent Literature 1 discloses a DP steel sheet in which the crystal grain diameter, volume fraction, and nanoindentation hardness of ferrite are controlled, and it is possible to achieve a high elongation (EL) and excellent bendability with this DP steel sheet.
- examples of a steel sheet having a high strength and a high elongation (EL) at the same time include TRIP steel sheet. Since this TRIP steel sheet has a steel sheet microstructure including retained austenite, a large elongation (EL) is achieved in the case where the steel sheet is deformed by work performed at a temperature equal to or higher than a temperature at which martensite transformation begins, because retained austenite transforms into martensite through transformation induced by stress.
- Patent Literature 2 discloses a TRIP steel sheet which includes bainitic ferrite in order to improve hole expansion capability.
- an object of certain embodiments of the present invention is, by solving the problems described above, to provide a high-strength cold-rolled steel sheet excellent in terms of elongation (EL) and hole expansion ratio ( ⁇ ) having a low yield ratio (YR) and a method for manufacturing the steel sheet.
- DP steel has a low yield ratio (YR).
- YR yield ratio
- voids are formed at its interface, in particular, its interface with soft ferrite when punching work is performed in a hole expansion process, the voids then combine with each other when the punched hole is expanded, and a crack occurs as the combination of the voids progresses. Therefore, there is a decrease in the hole expansion ratio ( ⁇ ) of DP steel.
- ⁇ hole expansion ratio
- retained austenite significantly increases elongation (EL)
- retained austenite since retained austenite, as is the case with hard martensite, causes the formation of voids when punching work is performed in a hole expansion process, there is a decrease in hole expansion ratio ( ⁇ ).
- EL elongation
- ⁇ hole expansion ratio
- Tempering conditions used for forming tempered martensite in order to increase hole expansion ratio ( ⁇ ) while achieving low yield ratio (YR) have been identified. Moreover, it is possible to inhibit the combination of voids in a hole expansion process by decreasing the average crystal grain diameter of retained austenite and tempered martensite in order to form a steel sheet microstructure in which retained austenite and tempered martensite are finely dispersed, which results in an increase in elongation (EL) and hole expansion ratio ( ⁇ ).
- fine martensite and retained austenite are formed by forming a microstructure composed of bainite and martensite in a first annealing process after cold rolling has been performed, by forming fine austenite through reverse transformation in a second annealing process, by then allowing bainite transformation to occur through cooling, and by then performing rapid cooling.
- a multi-phase microstructure including ferrite having an average crystal grain diameter of 5 ⁇ m or less in an amount of 30% to 55% in terms of volume fraction, retained austenite having an average crystal grain diameter of 2 ⁇ m or less in an amount of 5% to 15% in terms of volume fraction, and tempered martensite having an average crystal grain diameter of 2 ⁇ m or less in an amount of 30% to 60% in terms of volume fraction,
- the number of grains of the retained austenite existing in an area of 1000 ⁇ m 2 is 10 or more.
- the method including, after having performed hot rolling and cold rolling on a steel slab to obtain a cold-rolled steel sheet, performing continuous annealing on the cold-rolled steel sheet,
- a high-strength cold-rolled steel sheet refers to a cold-rolled steel sheet having a tensile strength (TS) of 980 MPa or more.
- an average cooling rate refers to a value derived by dividing a value derived by subtracting a cooling stop temperature from a cooling start temperature by a cooling time.
- an average heating rate refers to a value derived by dividing a value derived by subtracting a heating start temperature from a heating stop temperature by a heating time.
- TS tensile strength
- YR low yield ratio
- EL elongation
- ⁇ hole expansion ratio
- the high-strength, cold-rolled steel sheet according to the present invention has a chemical composition containing, by massa, C: 0.15% to 0.25%, Si: 1.0% to 2.0%, Mn: 1.8% to 2.5%, P: 0.10% or less, S: 0.010% or less, Al: 0.10% or less, N: 0.010% or less, and the balance being Fe and inevitable impurities, and a multi-phase microstructure including ferrite having an average crystal grain diameter of 5 ⁇ m or less in an amount of 30% to 55% in terms of volume fraction, retained austenite having an average crystal grain diameter of 2 ⁇ m or less in an amount of 5% to 15% in terms of volume fraction, and tempered martensite having an average crystal grain diameter of 2 ⁇ m or less in an amount of 30% to 60% in terms of volume fraction, in which the number of grains of the retained austenite existing in an area of 1000 ⁇ m 2 is 10 or more.
- % used when describing a chemical composition shall refer to “mass %”.
- C is a chemical element which is effective for increasing the strength of a steel sheet and which also contributes to the formation of second phases in embodiments of the present invention, that is, tempered martensite and retained austenite.
- the C content is set to be 0.15% or more, or preferably 0.18% or more.
- the C content is set to be 0.25% or less, or preferably 0.23% or less.
- a main phase refers to a ferrite phase
- second phases refers to a tempered martensite phase and a retained austenite phase
- the microstructure of the high-strength cold-rolled steel sheet according to embodiments of the present invention may include tempered bainite and pearlite.
- Si is a chemical element which is necessary for contributing to the formation of retained austenite by inhibiting the formation of carbides when bainite transformation occurs in the first and second annealing processes.
- the Si content is set to be 1.0% or more, or preferably 1.3% or more.
- the Si content is set to be 2.0% or less, or preferably 1.8% or less.
- Mn is a chemical element which contributes to an increase in strength through solid solution strengthening and by facilitating the formation of the second phases and which stabilizes austenite.
- the Mn content is set to be 1.8% or more.
- the Mn content is set to be 2.5% or less.
- the P content is set to be 0.10% or less, or preferably 0.05% or less.
- the S content is set to be 0.010% or less, or preferably 0.005% or less.
- the S content be 0.0005% or more.
- the Al content is set to be 0.10% or less, or preferably 0.08% or less.
- the Al content be 0.01% or more.
- the N content is set to be 0.010% or less, or preferably 0.006% or less.
- the remainder which is different from the constituent chemical elements described above is Fe and inevitable impurities.
- the inevitable impurities include Sb, Sn, Zn, and Co, and the acceptable ranges of the contents of these chemical elements are respectively Sb: 0.01% or less, Sn: 0.10% or less, Zn: 0.01% or less, and Co: 0. 10% or less.
- one, two, or more of the following chemical elements may be added in addition to the constituent chemical elements described above.
- V 0.10% or less
- V contributes to an increase in strength by forming fine carbonitrides
- V may be added as needed.
- the V content be 0.01% or more.
- the V content be 0.10% or less.
- Nb since V, contributes to an increase in strength by forming fine carbonitrides, Nb may be added as needed. In order to realize such an effect, it is preferable that the Nb content be 0.005% or more. On the other hand, there is a significant deterioration in elongation (EL) in the case where the Nb content is more than 0.10%. Therefore, it is preferable that the Nb content be 0.10% or less.
- Ti like V, contributes to an increase in strength by forming fine carbonitrides
- Ti may be added as needed. In order to realize such an effect, it is preferable that the Ti content be 0.005% or more. On the other hand, in the case where the Ti content is more than 0.10%, there is a significant deterioration in elongation (EL). Therefore, it is preferable that the Ti content be 0.10% or less.
- B is a chemical element which contributes to an increase in strength by increasing hardenability and by facilitating the formation of the second phases and which achieves hardenability without significantly increasing the hardness of tempered martensite
- B may be added as needed.
- the B content be 0.0003% or more.
- the B content be 0.010% or less.
- Cr is a chemical element which contributes to an increase in strength by facilitating the formation of the second phases
- Cr may be added as needed.
- the Cr content be 0.10% or more.
- the Cr content in the case where the Cr content is more than 0.50%, an excessive amount of tempered martensite is formed. Therefore, in the case where Cr is added, it is preferable that the Cr content be 0.50% or less.
- Mo is a chemical element which contributes to an increase in strength by facilitating the formation of the second phases and by partially forming carbides
- Mo may be added as needed. In order to realize such an effect, it is preferable that the Mo content be 0.05% or more. On the other hand, in the case where the Mo content is more than 0.50%, such an effect becomes saturated. Therefore, in the case where Mo is added, it is preferable that the Mo content be 0.50% or less.
- Cu is a chemical element which contributes to an increase in strength through solid solution strengthening and by facilitating the formation of the second phases
- Cu may be added as needed.
- the Cu content be 0.05% or more.
- the Cu content in the case where the Cu content is more than 0.50%, such an effect becomes saturated, and surface defects caused by Cu tend to occur. Therefore, in the case where Cu is added, it is preferable that the Cu content be 0.50% or less.
- Ni is, like Cu, a chemical element which contributes to an increase in strength through solid solution strengthening and by facilitating the formation of the second phases
- Ni may be added as needed.
- the Ni content be 0.05% or more.
- the Ni content is more than 0.50%, such effects become saturated. Therefore, in the case where Ni is added, it is preferable that the Ni content be 0.50% or less.
- Ca contributes to inhibiting a decrease in the hole expansion ratio ( ⁇ ) due to sulfides by spheroidizing the shape of sulfides
- Ca may be added as needed.
- the Ca content be 0.0005% or more.
- the Ca content in the case where the Ca content is more than 0.0050%, such an effect becomes saturated. Therefore, in the case where Ca is added, it is preferable that the Ca content be 0.0050% or less.
- REM since REM, like Ca, contributes to inhibiting a decrease in the hole expansion ratio ( ⁇ ) due to sulfides by spheroidizing the shape of sulfides, REM may be added as needed. In order to realize such an effect, it is preferable that the REM content be 0.0005% or more. On the other hand, in the case where the REM content is more than 0.0050%, such an effect becomes saturated. Therefore, in the case where REM is added, it is preferable that the REM content be 0.0050% or less.
- the high-strength cold-rolled steel sheet according to embodiments of the present invention includes ferrite, retained austenite, and tempered martensite.
- the high-strength cold-rolled steel sheet according to embodiments of the present invention may include tempered bainite as the remainder of the microstructure.
- the ferrite has an average crystal grain diameter of 5 ⁇ m or less and a volume fraction of 30% to 55%.
- the retained austenite has an average crystal grain diameter of 2 ⁇ m or less and a volume fraction of 5% to 15%.
- the tempered martensite has an average crystal grain diameter of 2 ⁇ m or less and a volume fraction of 30% to 60%.
- the number of grains of retained austenite having an average crystal grain diameter of 2 ⁇ m or less existing in an area of 1000 ⁇ m 2 is 10 or more.
- the term “a volume fraction” here shall refer to a volume fraction with respect to the whole steel sheet, and the same shall apply hereinafter.
- the volume fraction of ferrite described above is less than 30%, since there is an insufficient amount of soft ferrite, there is a decrease in elongation (EL). Therefore, the volume fraction of ferrite is set to be 30% or more, or preferably 35% or more. On the other hand, in the case where the volume fraction of ferrite is more than 55%, it is difficult to achieve a tensile strength (TS) of 980 MPa or more. Therefore, the volume fraction of ferrite is set to be 55% or less, or preferably 50% or less.
- the average crystal grain diameter of ferrite is set to be 5 ⁇ m or less.
- the volume fraction of retained austenite In order to achieve a high elongation (EL), it is necessary that the volume fraction of retained austenite be 5% to 15%. In the case where the volume fraction of retained austenite is less than 5%, it is not possible to achieve the desired elongation (EL). Therefore, the volume fraction of retained austenite is set to be 5% or more, or preferably 6% or more. On the other hand, in the case where the volume fraction of retained austenite is more than 15%, it is not possible to achieve the desired hole expansion ratio ( ⁇ ). Therefore, the volume fraction of retained austenite is set to be 15% or less, or preferably 12% or less. In addition, in order to achieve a high hole expansion ratio ( ⁇ ), the average crystal grain diameter of retained austenite is set to be 2 ⁇ m or less.
- the average crystal grain diameter of retained austenite is set to be 2 ⁇ m or less.
- the volume fraction of tempered martensite is set to be 30% to 60%. In the case where the volume fraction of tempered martensite is less than 30%, it is not possible to achieve a tensile strength of 980 MPa or more. On the other hand, in the case where the volume fraction of tempered martensite is more than 60%, it is difficult to achieve the desired elongation (EL). In addition, in order to achieve a high hole expansion ratio ( ⁇ ), the average crystal grain diameter of tempered martensite is set to be 2 ⁇ m or less.
- the average crystal grain diameter of tempered martensite is more than 2 ⁇ m, since voids which have been formed at the grain boundaries with ferrite tend to combine with each other, it is not possible to achieve the desired hole expansion ratio ( ⁇ ). Therefore, the upper limit of the average crystal grain diameter of tempered martensite is ,set to be 2 ⁇ m.
- tempered bainite may be partially formed in order to form retained austenite by allowing bainite transformation to occur in an annealing process.
- the volume fraction of this tempered bainite it is preferable that the volume fraction of tempered bainite be 30% or less in order to achieve a high elongation (EL).
- the number of grains of the above-described retained austenite having an average crystal grain diameter of 2 ⁇ m or less existing in an area of 1000 ⁇ m 2 be 10 or more. In the case where the number of grains of retained austenite existing in an area of 1000 ⁇ m 2 is less than 10, it is not possible to achieve the desired elongation (EL).
- the upper limit of the number of grains of retained austenite existing in an area of 1000 ⁇ m 2 in the case where the number of grains of retained austenite existing in an area of 1000 ⁇ m 2 is more than 50, voids which have been formed at the grain boundaries with ferrite tend to combine with each other. Therefore, it is preferable that the number of grains of retained austenite existing in an area of 1000 ⁇ m 2 be 50 or less.
- tempered bainite and pearlite are formed in addition to ferrite, retained austenite, and tempered martensite
- the volume fraction of pearlite be 5% or less.
- the volume fraction of tempered bainite be 30% or less.
- a SEM scanning electron microscope
- nital an alcohol solution containing nitric acid
- image analysis software Image-Pro ver. 7 produced by Media Cybernetics, Inc.
- the method for manufacturing the high-strength cold-rolled steel sheet according to embodiments of the present invention includes, after having performed hot rolling and cold rolling on a steel slab having the chemical composition (constituent chemical elements) described above, performing continuous annealing on the cold-rolled steel sheet, in which heating is performed to a temperature of 850° C. or higher, in which holding is performed at a first soaking temperature of 850° C. or higher for 30 seconds or more, in which cooling is then performed from the first soaking temperature to a second soaking temperature of 320° C. to 500° C. at a first average cooling rate of 3° C./s or more, in which holding is performed at the second soaking temperature of 320° C. to 500° C.
- cooling is then performed to a temperature of 100° C. or lower (for example, room temperature), in which heating is thereafter performed to a temperature of 750° C. or higher at an average heating rate of 3° C./s to 30° C./s, in which holding is performed at a third soaking temperature of 750° C. or higher for 30 seconds or more, in which cooling is then performed from the third soaking temperature to a temperature of 350° C. to 500° C. at a second average cooling rate of 3° C./s or more, in which cooling is performed to a temperature of 100° C. or lower at a third average cooling rate of 100° C./s to 1000° C./s, in which heating is performed to a temperature of 200° C. to 350° C., and in which holding is then performed at a fourth soaking temperature of 200° C. to 350° C. for 120 seconds to 1200 seconds.
- a temperature of 100° C. or lower for example, room temperature
- heating is thereafter performed to a temperature of 750° C. or higher
- the hot rolling process by performing rough rolling and finish rolling on a steel slab having the chemical composition described above after heating has been performed, a hot-rolled steel sheet is obtained.
- the steel slab used be manufactured by using a continuous casting method in order to prevent the macro segregation of the constituent chemical elements
- the slab may also be manufactured by using an ingot-making method or a thin-slab-casting method.
- the cast slab may not be reheated or may be reheated to a temperature of 1100° C. or higher.
- the slab in addition to a conventional method, in which, after having manufactured a steel slab, the slab is first cooled to a temperature of 100° C.
- an energy-saving process such as a hot direct rolling or a direct rolling, that is, a method in which a slab in the hot state is charged into a heating furnace without the slab having been cooled, a method in which a slab is rolled immediately after heat retention has been performed, or a method in which a slab in the cast state is rolled may be used without causing any problem.
- a slab heating temperature By controlling a slab heating temperature to be 1100° C. or higher, it is possible to decrease rolling load and to improve productivity. On the other hand, by controlling the slab heating temperature to be 1300° C. or lower, it is possible to decrease heating costs. Therefore, it is preferable that the slab heating temperature be 1100° C. to 1300° C.
- a finishing delivery temperature 830° C. or higher, since it is possible to finish hot rolling within an austenite single phase region, it is possible to inhibit a decrease in elongation (EL) and hole expansion ratio ( ⁇ ) due to an increase in the inhomogeneity of a microstructure in a steel sheet and the anisotropy of material properties after annealing.
- the finishing delivery temperature it is possible to inhibit deterioration in properties after annealing due to coarsening of a hot-rolled microstructure. Therefore, it is preferable that the finishing delivery temperature be 830° C. to 950° C.
- a coiling temperature by controlling a coiling temperature to be 700° C. or lower, since it is possible to inhibit the formation of coarse pearlite, it is possible to prevent a decrease in elongation (EL) and hole expansion ratio ( ⁇ ) after annealing has been performed. Therefore, it is preferable that the coiling temperature be 700° C. or lower, or more preferably 650° C. or lower.
- the coiling temperature be 400° C. or higher, since it is possible to inhibit the formation of excessive amounts of hard bainite and martensite, it is possible to decrease cold rolling load. Therefore, it is preferable that the coiling temperature be 400° C. or higher.
- pickling may be performed on the hot-rolled steel sheet after the hot rolling process described above. It is preferable that scale on the surface of the hot-rolled steel sheet be removed by performing pickling. There is no particular limitation on the method used for pickling, and pickling may be performed by using a commonly used method.
- cold rolling in which rolling is performed in order to obtain a cold-rolled steel sheet having a specified thickness
- cold rolling may be performed by using a commonly used method.
- intermediate annealing may be performed before the cold rolling process. By performing intermediate annealing, it is possible to decrease cold rolling load.
- annealing be performed at a temperature of 450° C. to 800° C. for 10 minutes to 50 hours.
- annealing is performed on the cold-rolled steel sheet.
- recrystallization is progressed, and retained austenite and tempered martensite are formed in a steel sheet microstructure in order to increase strength.
- ⁇ high hole expansion ratio
- a steel sheet microstructure including bainite, martensite, and retained austenite which are homogenized to some extent in the first annealing process it is possible to allow more homogeneous fine dispersion to occur in the second annealing process.
- tempering is performed after cooling is first performed to an excessive degree. With this, it is possible to achieve a high hole expansion ratio ( ⁇ ) while inhibiting a decrease in elongation (EL).
- heating is performed to a temperature of 850° C. or higher, holding is performed at a first soaking temperature of 850° C. or higher for 30 seconds or more, cooling is then performed from the first soaking temperature to a second soaking temperature of 320° C. to 500° C. at a first average cooling rate of 3° C./s or more, holding is performed at the second soaking temperature of 320° C. to 500° C. for 30 seconds or more, and cooling is then performed to a temperature of 100° C. or lower (for example, room temperature). Thereafter, in the second annealing process, heating is performed to a temperature of 750° C.
- holding is performed at a third soaking temperature of 750° C. or higher for 30 seconds or more, cooling is then performed from the third soaking temperature to a temperature of 350° C. to 500° C. at a second average cooling rate of 3° C./s or more, cooling is performed to a temperature of 100° C. or lower at a third average cooling rate of 100° C./s to 1000° C./s, heating is performed to a temperature of 200° C. to 350° C., and holding is then performed at a fourth soaking temperature of 200° C. to 350° C. for 120 seconds to 1200 seconds.
- the first soaking temperature is set to be a temperature in a temperature range in which an austenite single phase is formed.
- the first soaking temperature is lower than 850° C.
- the lower limit of the first soaking temperature is set to be 850° C., or preferably 870° C. or higher.
- the first soaking temperature be 1000° C.
- the holding time (soaking time) at the first soaking temperature is set to be 30 seconds or more.
- this holding time it is preferable that this holding time be 600 seconds or less in order to prevent coarse carbides from being formed in a steel sheet.
- the first annealing process in order to form a steel sheet microstructure including a large amount of bainite, cooling is performed to a second soaking temperature of 320° C. to 500° C. at a first average cooling rate of 3° C./s or more.
- the first average cooling rate is less than 3° C./s, since excessive amounts of ferrite, pearlite and spherical cementite are formed in a steel sheet microstructure, the lower limit of the first average cooling rate is set to be 3° C./s.
- the cooling stop temperature (hereinafter, also referred to as “second soaking temperature”) is lower than 320° C.
- the second soaking temperature is set to be 320° C. to 500° C., or preferably 350° C. to 450° C.
- the holding time at the second soaking temperature is set to be 30 seconds or more.
- cooling is performed to a temperature of 100° C. or lower (for example, room temperature). With this, it is possible to form a steel sheet microstructure including bainite.
- Heating to Third Soaking Temperature 750° C. or higher
- Average Heating Rate 3° C./s to 30° C./s
- the third soaking temperature is lower than 750° C., since there is an excessively small amount of austenite formed, it is not possible to achieve the desired volume fractions of martensite and retained austenite formed. Therefore, the third soaking temperature is set to be 750° C. or higher. In addition, it is preferable that the third soaking temperature be 900° C.
- the average heating rate to the third soaking temperature (750° C. or higher) is more than 30° C./s, recrystallization is less likely to progress. Therefore, the average heating rate is set to be 30° C./s or less. In addition, in the case where the average heating rate to the third soaking temperature (750° C. or higher) is less than 3° C./s, since ferrite grains are coarsened, it is not possible to achieve the specified average crystal grain diameter. Therefore, the average heating rate is set to be 3° C./s or more.
- the holding time at the third soaking temperature is set to be 30 seconds or more.
- cooling is performed to a temperature of 350° C. to 500° C. at a second average cooling rate of 3° C./s or more.
- the second average cooling rate is less than 3° C./s, excessive amounts of pearlite and spherical cementite are formed in a steel sheet microstructure. Therefore, the lower limit of the second average cooling rate is set to be 3° C./s.
- cooling at the second average cooling rate is performed to a temperature of lower than 350° C.
- the cooling at the second average cooling rate should be performed to a temperature of 500° C. or lower, or preferably 370° C. to 450° C.
- cooling is performed to a temperature of 100° C. or lower at a third average cooling rate of 100° C./s to 1000° C./s.
- the third average cooling rate is set to be 100° C./s or more.
- the third average cooling rate is set to be 1000° C./s or less.
- a tempering treatment is performed.
- This tempering is performed in order to improve workability by softening martensite. That is, after cooling is performed as described above, in order to temper martensite, after heating has been performed to a temperature of 200° C. to 350° C., holding is performed at a tempering temperature of 200° C. to 350° C. (hereinafter, also referred to as “fourth soaking temperature”) for 120 seconds to 1200 seconds.
- the tempering temperature (fourth soaking temperature) is lower than 200° C., since the softening of martensite is insufficient, there is a decrease in hole expansion capability. Therefore, the fourth soaking temperature is set to be 200° C. or higher.
- the tempering temperature (fourth soaking temperature) is higher than 350° C., there is an increase in yield ratio (YR). Therefore, the fourth soaking temperature is set to be 350° C. or lower, or preferably 300° C. or lower.
- the holding time at the fourth soaking temperature is set to be 120 seconds or more.
- the holding time at the fourth soaking temperature is set to be 1200 seconds or less.
- cooling method or cooling rate there is no limitation on cooling method or cooling rate.
- skin pass rolling may be performed after the annealing process. It is preferable that skin pass rolling be performed with an elongation ratio of 0.1% to 2.0%.
- a galvanized steel sheet may be manufactured by performing a galvanizing treatment in the annealing process, and a galvannealed steel sheet may be manufactured by performing an alloying treatment after a galvanizing treatment has been performed.
- an electroplated steel sheet may be manufactured.
- a steel sheet having a tensile strength (TS) of 980 MPa or more was judged as a high-strength steel sheet, a steel sheet having an elongation (EL) of 19% or more was judged as a steel sheet having a good elongation (EL), and a steel sheet having a yield ratio (YR) of 66% or less was judged as a steel sheet having the desired low yield ratio (YR).
- hole expansion capability in accordance with The Japan Iron and Steel Federation Standard (JFS T 1001 (1996), by punching a hole having a diameter of 10 mm ⁇ in a sample with a clearance of 12.5%, by setting the sample on a testing machine so that the burr was on the die side, and by forming the sample with a conical punch having a point angle of 60° , hole expansion ratio ( ⁇ ) was determined. A steel sheet having a ⁇ (%) of 30% or more was judged as a steel sheet having good hole expansion capability.
- steel sheet microstructure by using a SEM (scanning electron microscope), a TEM (transmission electron microscope), and an FE-SEM (field-emission-type scanning electron microscope), steel sheet microstructure was observed in order to identify ferrite, retained austenite, tempered martensite, and other kinds of steel microstructures.
- SEM scanning electron microscope
- TEM transmission electron microscope
- FE-SEM field-emission-type scanning electron microscope
- the volume fractions of ferrite and tempered martensite of the steel sheet were determined by polishing a cross section in the thickness direction parallel to the rolling direction of the steel sheet, by then etching the polished cross section through the use of a 3%-nital solution, by observing the etched cross section through the use of a SEM (scanning electron microscope) at magnifications of 2000 times and 5000 times, by determining the area fraction of each of the phases through the use of a point-counting method (in accordance with ASTM E562-83 (1988)), and by defining the area fraction as the volume fraction.
- SEM scanning electron microscope
- the average crystal grain diameters of ferrite, retained austenite, and tempered martensite since it was possible to calculate each area of the phases by inputting the steel sheet microstructure photographs, in which the crystal grains of ferrite, retained austenite, and tempered martensite had been identified in advance, into Image-Pro produced by Media Cybernetics, Inc., by calculating circle-equivalent diameters from the calculated areas, the average crystal grain diameter of each of the phases was defined as the average of the calculated circle-equivalent diameters.
- the volume fraction of retained austenite was determined by polishing the steel sheet in order to expose a surface located at 1 ⁇ 4 of the thickness of the steel sheet and by determining the X-ray diffraction intensities of the surface. By determining the integrated intensities of X-ray diffraction of.
- the number of grains of retained austenite were determined by counting the number in the observation of a steel sheet photograph taken through the use of a SEM.
- the hole expansion ratio ( ⁇ ) was less than 30%.
- the tensile strength (TS) was less than 980 MPa.
- the volume fraction of ferrite was more than 55%, where the average crystal grain diameter of ferrite was more than 5 ⁇ m, where the average crystal grain diameter of retained austenite was more than 2 ⁇ m, and where the volume fraction of tempered martensite was less than 30%
- the tensile strength (TS) was less than 980 MPa
- the yield ratio (YR) was more than 66%
- the hole expansion ratio ( ⁇ ) was less than 30%.
- the volume fraction of retained austenite was less than 5% and where the number of grains of retained austenite existing in an area of 1000 ⁇ m 2 was less than 10
- the elongation (EL) was less than 19%
- the yield ratio (YR) was more than 66%.
- the Si content was less than 1.0 mass %, where the volume fraction of retained austenite was less than 5%, and where the number of grains of retained austenite existing in an area of 1000 ⁇ m 2 was less than 10, the elongation (EL) was less than 19%.
- the Mn content was more than 2.5 mass %, where the average crystal grain diameter of retained austenite was more than 2 ⁇ m, where the volume fraction of tempered martensite was more than 60%, and where the average crystal grain diameter of tempered martensite was more than 2 ⁇ m, the elongation (EL) was less than 19%, the yield ratio (YR) was more than 66%, and the hole expansion ratio ( ⁇ ) was less than 30%.
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Abstract
Description
- This is the U.S. National Phase application of PCT/JP2015/006347, filed Dec. 21, 2015, which claims priority to Japanese Patent Application No. 2015-038506, filed Feb. 27, 2015, the disclosures of these applications being incorporated herein by reference in their entireties for all purposes.
- The present invention relates to a high-strength cold-rolled steel sheet having a high elongation (EL), a high hole expansion ratio (λ), and a low yield ratio (YR) and a method for manufacturing the steel sheet, and in particular, to a high-strength cold-rolled steel sheet which can be used for structural parts of, for example, an automobile.
- In a situation where an increase in fuel efficiency through the weight reduction of an automobile body is an important issue to be addressed in the automobile field, since there has been progress in reducing the thickness of automobile parts by using a high-strength steel sheet for automobile parts, there is a trend toward using a steel sheet having a tensile strength (TS) of 980 MPa or more. When a high-strength steel sheet which is used for the structural members and reinforcement members of an automobile is subjected to forming in order to obtain parts having complex shapes, the steel sheet is required to be excellent in terms of formability expressed not by a single property such as elongation (EL) or stretch flange formability (hereinafter, also referred to as “hole expansion capability”) but by both of the properties. Moreover, in the case where parts are assembled with high dimensional accuracy in order to form a module by performing, for example, arc welding or spot welding without allowing spring back or the like to occur after press forming has been performed, it is important that a steel sheet have a low yield ratio (YR) before work is performed. Here, the term “yield ratio (YR)” refers to the ratio of yield stress (YS) to tensile strength (TS), and YR is expressed as YR=YS/TS.
- Conventionally, examples of known high-strength cold-rolled steel sheet having satisfactory formability and a high strength at the same time include a dual-phase steel sheet (DP steel sheet), which has a multi-phase microstructure composed of ferrite and martensite. However, although a DP steel sheet has a high elongation (EL), a DP steel sheet has a disadvantage in that, since a crack tends to occur due to stress concentration occurring at the interface between ferrite and martensite, there is a deterioration in bendability and hole expansion capability. Therefore, for example, Patent Literature 1 discloses a DP steel sheet in which the crystal grain diameter, volume fraction, and nanoindentation hardness of ferrite are controlled, and it is possible to achieve a high elongation (EL) and excellent bendability with this DP steel sheet.
- In addition, examples of a steel sheet having a high strength and a high elongation (EL) at the same time include TRIP steel sheet. Since this TRIP steel sheet has a steel sheet microstructure including retained austenite, a large elongation (EL) is achieved in the case where the steel sheet is deformed by work performed at a temperature equal to or higher than a temperature at which martensite transformation begins, because retained austenite transforms into martensite through transformation induced by stress. However, in the case of this TRIP steel sheet, there is a disadvantage in that, since retained austenite transforms into martensite when punching work is performed, a crack occurs at the interface with ferrite, which results in a deterioration in hole expansion capability. Therefore, for example, Patent Literature 2 discloses a TRIP steel sheet which includes bainitic ferrite in order to improve hole expansion capability.
- PTL 1: Japanese Patent No. 4925611
- PTL 2: Japanese Patent No. 4716358
- However, since the steel sheet disclosed in Patent Literature 1 has an insufficient elongation (EL) in the case where it has a tensile strength (TS) of 980 MPa or more, it cannot be said that sufficient formability is achieved. In addition, since the steel sheet disclosed in Patent Literature 2 which utilizes retained austenite has a yield ratio (YR) of more than 66% in the case where it has a tensile strength (TS) of 980 MPa or more, spring back tends to occur after work has been performed. As described above, in the case of a high-strength steel sheet having a tensile strength (TS) of 980 MPa or more, it is difficult to achieve a high elongation (EL) and a high hole expansion ratio (λ), which are required for increasing press formability (hereinafter, also referred to as “formability”), while maintaining a low yield ratio (YR), and it is a fact that a steel sheet which is fully satisfactory in terms of these properties (yield ratio (YR), tensile strength (TS), elongation (EL), and hole expansion ratio (λ)) has not yet been developed.
- Therefore, an object of certain embodiments of the present invention is, by solving the problems described above, to provide a high-strength cold-rolled steel sheet excellent in terms of elongation (EL) and hole expansion ratio (λ) having a low yield ratio (YR) and a method for manufacturing the steel sheet.
- It is possible to achieve a high elongation (EL) and a high hole expansion ratio (λ) while maintaining a low yield ratio (YR) by controlling the crystal grain diameters and volume fractions of steel sheet microstructures, that is, ferrite, retained austenite, and tempered martensite.
- Generally, since movable dislocations are formed in ferrite when martensite transformation occurs in DP steel, DP steel has a low yield ratio (YR). However, since such martensite is hard, voids are formed at its interface, in particular, its interface with soft ferrite when punching work is performed in a hole expansion process, the voids then combine with each other when the punched hole is expanded, and a crack occurs as the combination of the voids progresses. Therefore, there is a decrease in the hole expansion ratio (λ) of DP steel. On the other hand, although there is an increase in hole expansion ratio (λ) by tempering martensite, there is also an increase in yield ratio (YR) at the same time. In addition, although retained austenite significantly increases elongation (EL), since retained austenite, as is the case with hard martensite, causes the formation of voids when punching work is performed in a hole expansion process, there is a decrease in hole expansion ratio (λ). As described above, it is conventionally difficult to improve the balance among elongation (EL), hole expansion ratio (λ), and yield ratio (YR).
- Tempering conditions used for forming tempered martensite in order to increase hole expansion ratio (λ) while achieving low yield ratio (YR) have been identified. Moreover, it is possible to inhibit the combination of voids in a hole expansion process by decreasing the average crystal grain diameter of retained austenite and tempered martensite in order to form a steel sheet microstructure in which retained austenite and tempered martensite are finely dispersed, which results in an increase in elongation (EL) and hole expansion ratio (λ). In order to realize such an effect, fine martensite and retained austenite are formed by forming a microstructure composed of bainite and martensite in a first annealing process after cold rolling has been performed, by forming fine austenite through reverse transformation in a second annealing process, by then allowing bainite transformation to occur through cooling, and by then performing rapid cooling. Moreover, by performing tempering on hard martensite in order to form tempered martensite, it is possible to obtain a steel sheet having a high elongation (EL) and a high hole expansion ratio (λ) while achieving a low yield ratio (YR).
- Certain embodiments of the present invention are as follows.
- [1] A high-strength, cold-rolled steel sheet having
- a chemical composition containing, by mass %, C: 0.15% to 0.25%, Si: 1.0% to 2.0%, Mn: 1.8% to 2.5%, P: 0.10% or less, S: 0.010% or less, Al: 0.10% or less, N: 0.010% or less, and the balance being Fe and inevitable impurities, and
- a multi-phase microstructure including ferrite having an average crystal grain diameter of 5 μm or less in an amount of 30% to 55% in terms of volume fraction, retained austenite having an average crystal grain diameter of 2 μm or less in an amount of 5% to 15% in terms of volume fraction, and tempered martensite having an average crystal grain diameter of 2 μm or less in an amount of 30% to 60% in terms of volume fraction,
- in which the number of grains of the retained austenite existing in an area of 1000 μm2 is 10 or more.
- [2] The high-strength, cold-rolled steel sheet according to item [1] above, in which the chemical composition further contains, by mass %, one or more selected from V: 0.10% or less, Nb: 0.10% or less, and Ti: 0.10% or less.
- [3] The high-strength, cold-rolled steel sheet according to item [1] or [2] above, in which the chemical composition further contains, by mass %, B: 0.010% or less.
- [4] The high-strength, cold-rolled steel sheet according to any one of items [1] to [3] above, in which the chemical composition further contains, by mass %, one or more selected from Cr: 0.50% or less, Mo: 0.50% or less, Cu: 0.50% or less, Ni: 0.50% or less, Ca: 0.0050% or less, and REM: 0.0050% or less.
- [5] A method for manufacturing the high-strength, cold-rolled steel sheet according to any one of items [1] to [4] above,
- the method including, after having performed hot rolling and cold rolling on a steel slab to obtain a cold-rolled steel sheet, performing continuous annealing on the cold-rolled steel sheet,
- the continuous annealing comprising:
- heating the cold-rolled steel sheet to a temperature of 850° C. or higher,
- holding the cold-rolled steel sheet at a first soaking temperature of 850° C. or higher for 30 seconds or more,
- then cooling the cold-rolled steel sheet from the first soaking temperature to a temperature of 320° C. to 500° C. at a first average cooling rate of 3° C./s or more,
- holding the cold-rolled steel sheet at a second soaking temperature of 320° C. to 500° C. for 30 seconds or more,
- then cooling the cold-rolled steel sheet to a temperature of 100° C. or lower,
- heating the cold-rolled steel sheet to a temperature of 750° C. or higher at an average heating rate of 3° C./s to 30° C./s,
- holding the cold-rolled steel sheet at a third soaking temperature of 750° C. or higher for 30 seconds or more,
- cooling the cold-rolled steel sheet from the third soaking temperature to a temperature of 350° C. to 500° C. at a second average cooling rate of 3° C./s or more,
- then cooling the cold-rolled steel sheet to a temperature of 100° C. or lower at a third average cooling rate of 100° C./s to 1000° C./s,
- heating the cold-rolled steel sheet to a temperature of 200° C. to 350° C., and
- then holding the cold-rolled steel sheet at a fourth soaking temperature of 200° C. to 350° C. for 120 seconds to 1200 seconds.
- In embodiments of the present invention, the term “a high-strength cold-rolled steel sheet” refers to a cold-rolled steel sheet having a tensile strength (TS) of 980 MPa or more.
- In addition, in embodiments of the present invention, the term “an average cooling rate” refers to a value derived by dividing a value derived by subtracting a cooling stop temperature from a cooling start temperature by a cooling time. In addition, the term “an average heating rate” refers to a value derived by dividing a value derived by subtracting a heating start temperature from a heating stop temperature by a heating time.
- According to embodiments of the present invention, by controlling the chemical composition and microstructure of a steel sheet, it is possible to stably obtain a high-strength cold-rolled steel sheet having a high elongation (EL) and a high hole expansion ratio (λ), that is, a high-strength cold-rolled steel sheet having a tensile strength (TS) of 980 MPa or more, a low yield ratio (YR) of 66% or less, an elongation (EL) of 19% or more, and a hole expansion ratio (λ) of 30% or more.
- Hereafter, embodiments of the present invention will be specifically described. The high-strength, cold-rolled steel sheet according to the present invention has a chemical composition containing, by massa, C: 0.15% to 0.25%, Si: 1.0% to 2.0%, Mn: 1.8% to 2.5%, P: 0.10% or less, S: 0.010% or less, Al: 0.10% or less, N: 0.010% or less, and the balance being Fe and inevitable impurities, and a multi-phase microstructure including ferrite having an average crystal grain diameter of 5 μm or less in an amount of 30% to 55% in terms of volume fraction, retained austenite having an average crystal grain diameter of 2 μm or less in an amount of 5% to 15% in terms of volume fraction, and tempered martensite having an average crystal grain diameter of 2 μm or less in an amount of 30% to 60% in terms of volume fraction, in which the number of grains of the retained austenite existing in an area of 1000 μm2 is 10 or more.
- First, the reasons for the limitations on the chemical element of the high-strength cold-rolled steel sheet according to embodiments of the present invention will be described. Hereinafter, “%” used when describing a chemical composition shall refer to “mass %”.
- C: 0.15% to 0.25%
- C is a chemical element which is effective for increasing the strength of a steel sheet and which also contributes to the formation of second phases in embodiments of the present invention, that is, tempered martensite and retained austenite. In the case where the C content is less than 0.15%, since it is difficult to control the volume fraction of tempered martensite to be 30% or more or the volume fraction of retained austenite to be 5% or more, it is difficult to control tensile strength (TS) to be 980 MPa or more. Therefore, the C content is set to be 0.15% or more, or preferably 0.18% or more. On the other hand, in the case where the C content is more than 0.25%, since there is an increase in the difference in hardness between ferrite and tempered martensite, it is not possible to achieve the desired hole expansion ratio W. Therefore, the C content is set to be 0.25% or less, or preferably 0.23% or less.
- Here, in the case of the high-strength cold-rolled steel sheet according to embodiments of the present invention, the term “a main phase” refers to a ferrite phase, and the term “second phases” described above refers to a tempered martensite phase and a retained austenite phase. In addition, the microstructure of the high-strength cold-rolled steel sheet according to embodiments of the present invention may include tempered bainite and pearlite.
- Si: 1.0% to 2.0%
- Si is a chemical element which is necessary for contributing to the formation of retained austenite by inhibiting the formation of carbides when bainite transformation occurs in the first and second annealing processes. In the case where the Si content is less than 1.0%, it is not possible to form a sufficient amount of retained austenite. Therefore, the Si content is set to be 1.0% or more, or preferably 1.3% or more. On the other hand, in the case where the Si content is more than 2.0%, since the volume fraction of ferrite becomes more than 55%, and since the average crystal grain diameter becomes more than 5 μm, it is not possible to achieve a tensile strength (TS) of 980 MPa or more or a sufficient hole expansion ratio (λ). Therefore, the Si content is set to be 2.0% or less, or preferably 1.8% or less.
- Mn: 1.8% to 2.5%
- Mn is a chemical element which contributes to an increase in strength through solid solution strengthening and by facilitating the formation of the second phases and which stabilizes austenite. In the case where the Mn content is less than 1.8%, it is not possible to control the volume fraction of the second phases to be within the desired ranges. Therefore, the Mn content is set to be 1.8% or more. On the other hand, in the case where the Mn content is more than 2.5%, since the volume fraction of tempered martensite becomes more than 60%, and since there is an increase in the hardness of tempered martensite, it is not possible to achieve the desired hole expansion ratio (λ). Therefore, the Mn content is set to be 2.5% or less.
- P: 0.10% or less
- Although P contributes to an increase in strength through solid solution strengthening, in the case where the P content is more than 0.10%, since the segregation of P significantly occurs at the grain boundaries, a grain-boundary crack occurs due to the embrittlement of the grain boundaries, which makes it impossible to achieve the desired hole expansion ratio (λ). Therefore, the P content is set to be 0.10% or less, or preferably 0.05% or less.
- S: 0.010% or less
- In the case where the S content is more than 0.010%, since large amounts of sulfides such as MnS are formed, voids are formed around the sulfides when punching is performed in a hole expansion test, which makes it impossible to achieve the desired hole expansion ratio (λ). Therefore, the S content is set to be 0.010% or less, or preferably 0.005% or less. On the other hand, although there is no particular limitation on the lower limit of the S content, there is an increase in steel-making costs in order to control the S content to be very small, that is, less than 0.0005%. Therefore, it is preferable that the S content be 0.0005% or more.
- Al: 0.10% or less
- Although Al is a chemical element which is necessary for deoxidation, in the case where the Al content is more than 0.10%, this deoxidation effect becomes saturated. Therefore, the Al content is set to be 0.10% or less, or preferably 0.08% or less. On the other hand, in order to realize this deoxidation effect, it is preferable that the Al content be 0.01% or more.
- N: 0.010% or less
- Since N decreases the hole expansion ratio (λ) by forming coarse nitrides, it is necessary to decrease the N content. In the case where the N content is more than 0.010%, it is not possible to achieve the desired hole expansion ratio (λ). Therefore, the N content is set to be 0.010% or less, or preferably 0.006% or less.
- The remainder which is different from the constituent chemical elements described above is Fe and inevitable impurities. Examples of the inevitable impurities include Sb, Sn, Zn, and Co, and the acceptable ranges of the contents of these chemical elements are respectively Sb: 0.01% or less, Sn: 0.10% or less, Zn: 0.01% or less, and Co: 0. 10% or less.
- In addition, even in the case where Ta, Mg, and Zr are added in amounts within the ranges which are common among ordinary steel chemical compositions, there is no decrease in the effects of certain embodiments of the present invention.
- In addition, in embodiments of the present invention, one, two, or more of the following chemical elements may be added in addition to the constituent chemical elements described above.
- V: 0.10% or less
- Since V contributes to an increase in strength by forming fine carbonitrides, V may be added as needed. In order to realize such an effect, it is preferable that the V content be 0.01% or more. On the other hand, in the case where the V content is large, there is only a small increase in the effect of increasing strength corresponding to an increase in V content in the case where the V content is more than 0.10%, and there is an increase in alloy costs. Therefore, in the case where V is added, it is preferable that the V content be 0.10% or less.
- Nb: 0.10% or less
- Since Nb, like V, contributes to an increase in strength by forming fine carbonitrides, Nb may be added as needed. In order to realize such an effect, it is preferable that the Nb content be 0.005% or more. On the other hand, there is a significant deterioration in elongation (EL) in the case where the Nb content is more than 0.10%. Therefore, it is preferable that the Nb content be 0.10% or less.
- Ti: 0.10% or less
- Since Ti, like V, contributes to an increase in strength by forming fine carbonitrides, Ti may be added as needed. In order to realize such an effect, it is preferable that the Ti content be 0.005% or more. On the other hand, in the case where the Ti content is more than 0.10%, there is a significant deterioration in elongation (EL). Therefore, it is preferable that the Ti content be 0.10% or less.
- B: 0.010% or less
- Since B is a chemical element which contributes to an increase in strength by increasing hardenability and by facilitating the formation of the second phases and which achieves hardenability without significantly increasing the hardness of tempered martensite, B may be added as needed. In order to realize such effects, it is preferable that the B content be 0.0003% or more. On the other hand, in the case where the B content is more than 0.010%, such effects become saturated. Therefore, it is preferable that the B content be 0.010% or less.
- Cr: 0.50% or less
- Since Cr is a chemical element which contributes to an increase in strength by facilitating the formation of the second phases, Cr may be added as needed. In order to realize such an effect, it is preferable that the Cr content be 0.10% or more. On the other hand, in the case where the Cr content is more than 0.50%, an excessive amount of tempered martensite is formed. Therefore, in the case where Cr is added, it is preferable that the Cr content be 0.50% or less.
- Mo: 0.50% or less
- Since Mo is a chemical element which contributes to an increase in strength by facilitating the formation of the second phases and by partially forming carbides, Mo may be added as needed. In order to realize such an effect, it is preferable that the Mo content be 0.05% or more. On the other hand, in the case where the Mo content is more than 0.50%, such an effect becomes saturated. Therefore, in the case where Mo is added, it is preferable that the Mo content be 0.50% or less.
- Cu: 0.50% or less
- Since Cu is a chemical element which contributes to an increase in strength through solid solution strengthening and by facilitating the formation of the second phases, Cu may be added as needed. In order to realize such an effect, it is preferable that the Cu content be 0.05% or more. On the other hand, in the case where the Cu content is more than 0.50%, such an effect becomes saturated, and surface defects caused by Cu tend to occur. Therefore, in the case where Cu is added, it is preferable that the Cu content be 0.50% or less.
- Ni: 0.50% or less
- Since Ni is, like Cu, a chemical element which contributes to an increase in strength through solid solution strengthening and by facilitating the formation of the second phases, Ni may be added as needed. In order to realize such an effect, it is preferable that the Ni content be 0.05% or more. In addition, in the case where Ni is added in combination with Cu, since Ni is effective for inhibiting surface defects caused by Cu from occurring, adding Ni is effective when Cu is added. On the other hand, in the case where the Ni content is more than 0.50%, such effects become saturated. Therefore, in the case where Ni is added, it is preferable that the Ni content be 0.50% or less.
- Ca: 0.0050% or less
- Since Ca contributes to inhibiting a decrease in the hole expansion ratio (λ) due to sulfides by spheroidizing the shape of sulfides, Ca may be added as needed. In order to realize such an effect, it is preferable that the Ca content be 0.0005% or more. On the other hand, in the case where the Ca content is more than 0.0050%, such an effect becomes saturated. Therefore, in the case where Ca is added, it is preferable that the Ca content be 0.0050% or less.
- REM: 0.0050% or less
- Since REM, like Ca, contributes to inhibiting a decrease in the hole expansion ratio (λ) due to sulfides by spheroidizing the shape of sulfides, REM may be added as needed. In order to realize such an effect, it is preferable that the REM content be 0.0005% or more. On the other hand, in the case where the REM content is more than 0.0050%, such an effect becomes saturated. Therefore, in the case where REM is added, it is preferable that the REM content be 0.0050% or less.
- Hereafter, the microstructure of the high-strength cold-rolled steel sheet according to embodiments of the present invention will be described in detail. The high-strength cold-rolled steel sheet according to embodiments of the present invention includes ferrite, retained austenite, and tempered martensite. In addition, the high-strength cold-rolled steel sheet according to embodiments of the present invention may include tempered bainite as the remainder of the microstructure. The ferrite has an average crystal grain diameter of 5 μm or less and a volume fraction of 30% to 55%. In addition, the retained austenite has an average crystal grain diameter of 2 μm or less and a volume fraction of 5% to 15%. In addition, the tempered martensite has an average crystal grain diameter of 2 μm or less and a volume fraction of 30% to 60%. In addition, in the case of the high-strength cold-rolled steel sheet according to embodiments of the present invention, the number of grains of retained austenite having an average crystal grain diameter of 2 μm or less existing in an area of 1000 μm2 is 10 or more. The term “a volume fraction” here shall refer to a volume fraction with respect to the whole steel sheet, and the same shall apply hereinafter.
- In the case where the volume fraction of ferrite described above is less than 30%, since there is an insufficient amount of soft ferrite, there is a decrease in elongation (EL). Therefore, the volume fraction of ferrite is set to be 30% or more, or preferably 35% or more. On the other hand, in the case where the volume fraction of ferrite is more than 55%, it is difficult to achieve a tensile strength (TS) of 980 MPa or more. Therefore, the volume fraction of ferrite is set to be 55% or less, or preferably 50% or less. In addition, in the case where the average crystal grain diameter of ferrite is more than 5 μm, since voids which have been formed in a punched end surface in a hole expansion process tend to combine with each other when the punched hole is expanded, it is not possible to achieve the desired hole expansion ratio (?). Moreover, in the case where the average crystal grain diameter of ferrite is more than 5 μm, it is not possible to achieve a yield ratio (YR) of less than the desired value. Therefore, the average crystal grain diameter of ferrite is set to be 5 μm or less.
- In order to achieve a high elongation (EL), it is necessary that the volume fraction of retained austenite be 5% to 15%. In the case where the volume fraction of retained austenite is less than 5%, it is not possible to achieve the desired elongation (EL). Therefore, the volume fraction of retained austenite is set to be 5% or more, or preferably 6% or more. On the other hand, in the case where the volume fraction of retained austenite is more than 15%, it is not possible to achieve the desired hole expansion ratio (λ). Therefore, the volume fraction of retained austenite is set to be 15% or less, or preferably 12% or less. In addition, in order to achieve a high hole expansion ratio (λ), the average crystal grain diameter of retained austenite is set to be 2 μm or less. In the case where the average crystal grain diameter of retained austenite is more than 2 μm, voids tend to combine with each other after the voids have been formed in a hole expansion process. Therefore, the average crystal grain diameter of retained austenite is set to be 2 μm or less.
- In order to achieve a tensile strength of 980 MPa or more while achieving the desired hole expansion ratio (λ) and low yield ratio (YR), the volume fraction of tempered martensite is set to be 30% to 60%. In the case where the volume fraction of tempered martensite is less than 30%, it is not possible to achieve a tensile strength of 980 MPa or more. On the other hand, in the case where the volume fraction of tempered martensite is more than 60%, it is difficult to achieve the desired elongation (EL). In addition, in order to achieve a high hole expansion ratio (λ), the average crystal grain diameter of tempered martensite is set to be 2 μm or less. In the case where the average crystal grain diameter is more than 2 μm, since voids which have been formed at the grain boundaries with ferrite tend to combine with each other, it is not possible to achieve the desired hole expansion ratio (λ). Therefore, the upper limit of the average crystal grain diameter of tempered martensite is ,set to be 2 μm.
- In addition, in a steel sheet microstructure, tempered bainite may be partially formed in order to form retained austenite by allowing bainite transformation to occur in an annealing process. Although there is no particular limitation on the volume fraction of this tempered bainite, it is preferable that the volume fraction of tempered bainite be 30% or less in order to achieve a high elongation (EL).
- Moreover, in order to achieve a high elongation (EL), it is necessary that the number of grains of the above-described retained austenite having an average crystal grain diameter of 2 μm or less existing in an area of 1000 μm2 be 10 or more. In the case where the number of grains of retained austenite existing in an area of 1000 μm2 is less than 10, it is not possible to achieve the desired elongation (EL). On the other hand, although there is no particular limitation on the upper limit of the number of grains of retained austenite existing in an area of 1000 μm2, in the case where the number of grains of retained austenite existing in an area of 1000 μm2 is more than 50, voids which have been formed at the grain boundaries with ferrite tend to combine with each other. Therefore, it is preferable that the number of grains of retained austenite existing in an area of 1000 μm2 be 50 or less.
- In addition, in the case of the steel sheet according to embodiments of the present invention, although there is a case where tempered bainite and pearlite are formed in addition to ferrite, retained austenite, and tempered martensite, it is possible to achieve an object of the present invention as long as the above-described conditions regarding the volume fractions and average crystal grain diameters of ferrite, retained austenite, and tempered martensite and the number of grains of retained austenite existing in an area of 1000 μm2 are satisfied. However, it is preferable that the volume fraction of pearlite be 5% or less. In addition, as described above, it is preferable that the volume fraction of tempered bainite be 30% or less.
- Here, it is possible to observe the multi-phase microstructure of a steel sheet described above by using, for example, a SEM (scanning electron microscope). Specifically, first, a cross section in the thickness direction parallel to the rolling direction of a steel sheet is polished and then etched by using nital (an alcohol solution containing nitric acid). Subsequently, by taking microstructure photographs through the use of a scanning electron microscope at magnifications of 2000 times and 5000 times, by extracting desired regions in the obtained microstructure photograph data through image analysis, it is possible to identify ferrite, retained austenite, tempered martensite, or tempered bainite through the use of image analysis software (Image-Pro ver. 7 produced by Media Cybernetics, Inc.).
- It is possible to determine the above-described desired volume fractions of ferrite, retained austenite, and tempered martensite by determining the area ratios of these phases through the use of a point-counting method (in accordance with ASTM E562-83 (1988)) and by defining the area ratios as the volume fractions. In addition, it is possible to determine the above-described desired average crystal grain diameters of ferrite, retained austenite, and tempered martensite by calculating the circle-equivalent diameters of these phases from a steel sheet microstructure photograph and by calculating the average values of the circle-equivalent diameters. In addition, it is possible to determine the number of grains of retained austenite by counting in the observation of a steel sheet microstructure photograph.
- In addition, it is possible to control the above-described desired volume fractions and average crystal grain diameters of ferrite, retained austenite, and tempered martensite and the number of grains of retained austenite by controlling a steel sheet microstructure when the first annealing is performed and/or when the second annealing is performed.
- Hereafter, the method for manufacturing the high-strength cold-rolled steel sheet according to embodiments of the present invention will be described.
- The method for manufacturing the high-strength cold-rolled steel sheet according to embodiments of the present invention includes, after having performed hot rolling and cold rolling on a steel slab having the chemical composition (constituent chemical elements) described above, performing continuous annealing on the cold-rolled steel sheet, in which heating is performed to a temperature of 850° C. or higher, in which holding is performed at a first soaking temperature of 850° C. or higher for 30 seconds or more, in which cooling is then performed from the first soaking temperature to a second soaking temperature of 320° C. to 500° C. at a first average cooling rate of 3° C./s or more, in which holding is performed at the second soaking temperature of 320° C. to 500° C. for 30 seconds or more, in which cooling is then performed to a temperature of 100° C. or lower (for example, room temperature), in which heating is thereafter performed to a temperature of 750° C. or higher at an average heating rate of 3° C./s to 30° C./s, in which holding is performed at a third soaking temperature of 750° C. or higher for 30 seconds or more, in which cooling is then performed from the third soaking temperature to a temperature of 350° C. to 500° C. at a second average cooling rate of 3° C./s or more, in which cooling is performed to a temperature of 100° C. or lower at a third average cooling rate of 100° C./s to 1000° C./s, in which heating is performed to a temperature of 200° C. to 350° C., and in which holding is then performed at a fourth soaking temperature of 200° C. to 350° C. for 120 seconds to 1200 seconds.
- [Hot Rolling Process]
- In the hot rolling process, by performing rough rolling and finish rolling on a steel slab having the chemical composition described above after heating has been performed, a hot-rolled steel sheet is obtained. Although it is preferable that the steel slab used be manufactured by using a continuous casting method in order to prevent the macro segregation of the constituent chemical elements, the slab may also be manufactured by using an ingot-making method or a thin-slab-casting method. Regarding preferable hot rolling conditions, first, the cast slab may not be reheated or may be reheated to a temperature of 1100° C. or higher. In embodiments of the present invention, in addition to a conventional method, in which, after having manufactured a steel slab, the slab is first cooled to a temperature of 100° C. or lower (for example room temperature) and then reheated, an energy-saving process such as a hot direct rolling or a direct rolling, that is, a method in which a slab in the hot state is charged into a heating furnace without the slab having been cooled, a method in which a slab is rolled immediately after heat retention has been performed, or a method in which a slab in the cast state is rolled may be used without causing any problem.
- By controlling a slab heating temperature to be 1100° C. or higher, it is possible to decrease rolling load and to improve productivity. On the other hand, by controlling the slab heating temperature to be 1300° C. or lower, it is possible to decrease heating costs. Therefore, it is preferable that the slab heating temperature be 1100° C. to 1300° C.
- In addition, by controlling a finishing delivery temperature to be 830° C. or higher, since it is possible to finish hot rolling within an austenite single phase region, it is possible to inhibit a decrease in elongation (EL) and hole expansion ratio (λ) due to an increase in the inhomogeneity of a microstructure in a steel sheet and the anisotropy of material properties after annealing. On the other hand, by controlling the finishing delivery temperature to be 950° C. or lower, it is possible to inhibit deterioration in properties after annealing due to coarsening of a hot-rolled microstructure. Therefore, it is preferable that the finishing delivery temperature be 830° C. to 950° C.
- There is no particular limitation on the method used for cooling the hot-rolled steel sheet after hot rolling. Also, there is no particular limitation on a coiling temperature.
- However, by controlling a coiling temperature to be 700° C. or lower, since it is possible to inhibit the formation of coarse pearlite, it is possible to prevent a decrease in elongation (EL) and hole expansion ratio (λ) after annealing has been performed. Therefore, it is preferable that the coiling temperature be 700° C. or lower, or more preferably 650° C. or lower. On the other hand, although there is no particular limitation on the lower limit of the coiling temperature, by controlling the coiling temperature to be 400° C. or higher, since it is possible to inhibit the formation of excessive amounts of hard bainite and martensite, it is possible to decrease cold rolling load. Therefore, it is preferable that the coiling temperature be 400° C. or higher.
- [Pickling Process]
- In the method for manufacturing the high-strength cold-rolled steel sheet according to embodiments of the present invention, pickling may be performed on the hot-rolled steel sheet after the hot rolling process described above. It is preferable that scale on the surface of the hot-rolled steel sheet be removed by performing pickling. There is no particular limitation on the method used for pickling, and pickling may be performed by using a commonly used method.
- [Cold Rolling Process]
- In the method for manufacturing the high-strength cold-rolled steel sheet according to embodiments of the present invention, after hot rolling has been performed on the steel slab described above, or after pickling has been performed on the hot-rolled steel sheet, cold rolling, in which rolling is performed in order to obtain a cold-rolled steel sheet having a specified thickness, is performed. There is no particular limitation on the cold rolling process, and cold rolling may be performed by using a commonly used method. In addition, intermediate annealing may be performed before the cold rolling process. By performing intermediate annealing, it is possible to decrease cold rolling load. Although there is no particular limitation on the time or the temperature of the intermediate annealing, in the case where batch annealing is performed on a steel sheet in a coiled state, for example, it is preferable that annealing be performed at a temperature of 450° C. to 800° C. for 10 minutes to 50 hours.
- [Annealing Process]
- In the method for manufacturing the high-strength cold-rolled steel sheet according to embodiments of the present invention, after cold rolling as described above, annealing is performed on the cold-rolled steel sheet. In the annealing process, recrystallization is progressed, and retained austenite and tempered martensite are formed in a steel sheet microstructure in order to increase strength. In addition, in the method for manufacturing the high-strength cold-rolled steel sheet according to embodiments of the present invention, by performing annealing twice, since it is possible to make fine crystal grains of tempered martensite and retained austenite after annealing, it is possible to achieve a high hole expansion ratio (λ). By allowing untransformed austenite to transform into bainite during a cooling process in the first annealing process, large amounts of fine retained austenite and martensite are retained. However, since the crystal grain diameter of martensite is still large after only the first annealing process has been performed, it is not possible to achieve the desired hole expansion ratio (λ). Therefore, the second annealing is performed in order to further make fine crystal grains of martensite. With this, since martensite and retained austenite, which have been formed in the first annealing process, become the nucleation sites of austenite which is formed through reverse transformation in the second annealing process, it is possible to perform cooling while maintaining fine phases in the second annealing process. That is, by forming a steel sheet microstructure including bainite, martensite, and retained austenite which are homogenized to some extent in the first annealing process, it is possible to allow more homogeneous fine dispersion to occur in the second annealing process. In order to form tempered martensite in the second annealing process, tempering is performed after cooling is first performed to an excessive degree. With this, it is possible to achieve a high hole expansion ratio (λ) while inhibiting a decrease in elongation (EL).
- Therefore, in the first annealing process, heating is performed to a temperature of 850° C. or higher, holding is performed at a first soaking temperature of 850° C. or higher for 30 seconds or more, cooling is then performed from the first soaking temperature to a second soaking temperature of 320° C. to 500° C. at a first average cooling rate of 3° C./s or more, holding is performed at the second soaking temperature of 320° C. to 500° C. for 30 seconds or more, and cooling is then performed to a temperature of 100° C. or lower (for example, room temperature). Thereafter, in the second annealing process, heating is performed to a temperature of 750° C. or higher at an average heating rate of 3° C./s to 30° C./s, holding is performed at a third soaking temperature of 750° C. or higher for 30 seconds or more, cooling is then performed from the third soaking temperature to a temperature of 350° C. to 500° C. at a second average cooling rate of 3° C./s or more, cooling is performed to a temperature of 100° C. or lower at a third average cooling rate of 100° C./s to 1000° C./s, heating is performed to a temperature of 200° C. to 350° C., and holding is then performed at a fourth soaking temperature of 200° C. to 350° C. for 120 seconds to 1200 seconds.
- <First Annealing Process>
- (Heating to First Soaking Temperature (850° C. or Higher) and Holding for 30 Seconds or More)
- In the first annealing process, heating is firstly performed to the first soaking temperature. This first soaking temperature is set to be a temperature in a temperature range in which an austenite single phase is formed. In the case where the first soaking temperature is lower than 850° C., since there is a decrease in the amount of bainite after the first annealing process, there is an increase in the crystal grain diameter of tempered martensite and retained austenite which are formed in the second annealing process, which results in a decrease in hole expansion ratio (λ). Therefore, the lower limit of the first soaking temperature is set to be 850° C., or preferably 870° C. or higher. In addition, it is preferable that the first soaking temperature be 1000° C. or lower in order to prevent the crystal grain diameter of austenite from increasing. In addition, in order to allow recrystallization to progress and in order to allow the all or part of the grains to transform into austenite, the holding time (soaking time) at the first soaking temperature is set to be 30 seconds or more. Although there is no particular limitation on the upper limit of this holding time, it is preferable that this holding time be 600 seconds or less in order to prevent coarse carbides from being formed in a steel sheet.
- (Cooling from First Soaking Temperature to Second Soaking Temperature (320° C. to 500° C.) at First Average Cooling Rate (3° C./s or More))
- In the first annealing process, in order to form a steel sheet microstructure including a large amount of bainite, cooling is performed to a second soaking temperature of 320° C. to 500° C. at a first average cooling rate of 3° C./s or more. In the case where the first average cooling rate is less than 3° C./s, since excessive amounts of ferrite, pearlite and spherical cementite are formed in a steel sheet microstructure, the lower limit of the first average cooling rate is set to be 3° C./s. In addition, in the case where the cooling stop temperature (hereinafter, also referred to as “second soaking temperature”) is lower than 320° C., since an excessive amount of massive martensite is formed in the cooling process, it is difficult to form a fine homogeneous steel sheet microstructure in the second annealing process, which makes it impossible to achieve the desired hole expansion ratio (λ). In the case where the cooling stop temperature (second soaking temperature) is higher than 500° C., since there is an excessive increase in the amount of pearlite, it is difficult to form a fine homogeneous steel sheet microstructure in the second annealing process, which makes it impossible to achieve the desired hole expansion ratio (λ). Therefore, the second soaking temperature is set to be 320° C. to 500° C., or preferably 350° C. to 450° C.
- (Holding at Second Soaking Temperature for 30 Seconds or More)
- By allowing untransformed austenite to transform into bainite, bainite and retained austenite are formed. In the case where holding time at the second soaking temperature is less than 30 seconds, since there is an increase in the amount of untransformed austenite, there is an increase in the amount of massive martensite in a steel sheet microstructure after the first annealing process, which makes it impossible to make fine crystal grains of a steel sheet microstructure after the second annealing process. Therefore, the holding time at the second soaking temperature is set to be 30 seconds or more.
- (Cooling to a Temperature of 100° C. or Lower)
- After holding has been performed at the second soaking temperature, cooling is performed to a temperature of 100° C. or lower (for example, room temperature). With this, it is possible to form a steel sheet microstructure including bainite.
- <Second Annealing Process>
- (Heating to Third Soaking Temperature (750° C. or higher) at an Average Heating Rate of 3° C./s to 30° C./s)
- In the second annealing process, by forming the nucleation sites of ferrite and austenite which are formed by recrystallization due to reverse transformation, and by controlling the speed of the formation of the nucleation sites of recrystallized ferrite to be larger than that of coarsening of the nucleation sites in order to grow grains, it is possible to make the crystal grains fine after the annealing process. In the case where the third soaking temperature is lower than 750° C., since there is an excessively small amount of austenite formed, it is not possible to achieve the desired volume fractions of martensite and retained austenite formed. Therefore, the third soaking temperature is set to be 750° C. or higher. In addition, it is preferable that the third soaking temperature be 900° C. or lower in order to remove the influence of the steel sheet microstructure which has been formed in the first annealing process by performing annealing in an austenite single phase region is formed. In addition, in the case where the average heating rate to the third soaking temperature (750° C. or higher) is more than 30° C./s, recrystallization is less likely to progress. Therefore, the average heating rate is set to be 30° C./s or less. In addition, in the case where the average heating rate to the third soaking temperature (750° C. or higher) is less than 3° C./s, since ferrite grains are coarsened, it is not possible to achieve the specified average crystal grain diameter. Therefore, the average heating rate is set to be 3° C./s or more.
- (Holding at Third Soaking Temperature for 30 Seconds or More)
- In the second annealing process, holding is performed at a third soaking temperature of 750° C. or higher for 30 seconds or more. In the case where the holding time at the third soaking temperature is less than 30 seconds, since insufficient amounts of chemical elements such as Mn are concentrated in austenite, and crystal grains of untransformed austenite are coarsened in the cooling process, it is impossible to achieve the desired hole expansion ratio (λ). Therefore, the holding time at the third soaking temperature is set to be 30 seconds or more.
- (Cooling from Third Soaking Temperature to a Temperature of 350° C. to 500° C. at Second Average Cooling Rate (3° C./s or More))
- In order to increase elongation (EL) by forming retained austenite, since it is necessary that the concentration of C and Mn in untransformed austenite and bainite transformation be promoted in a cooling process from the third soaking temperature, cooling is performed to a temperature of 350° C. to 500° C. at a second average cooling rate of 3° C./s or more. In the case where the second average cooling rate is less than 3° C./s, excessive amounts of pearlite and spherical cementite are formed in a steel sheet microstructure. Therefore, the lower limit of the second average cooling rate is set to be 3° C./s. In addition, in the case where cooling at the second average cooling rate is performed to a temperature of lower than 350° C., since an excessive amount of martensite is formed in the cooling process, and the amounts of bainite transformation and retained austenite are decreased due to a decrease in the amount of untransformed austenite, it is impossible to achieve the desired elongation (EL). Therefore, cooling at the second average cooling rate should be performed to a temperature of 350° C. or higher. On the other hand, in the case where cooling at the second average cooling rate is performed to a temperature of higher than 500° C., since insufficient amounts of C and Mn are concentrated in untransformed austenite, there is a decrease in the amount of retained austenite formed in the final steel sheet microstructure, which makes it impossible to achieve the desired elongation (EL). Therefore, the cooling at the second average cooling rate should be performed to a temperature of 500° C. or lower, or preferably 370° C. to 450° C.
- (Cooling to a Tmperature of 100° C. or Lower at a Third Average Cooling Rate of 100° C./s to 1000° C./s)
- Subsequently, in order to form fine martensite and retained austenite, cooling is performed to a temperature of 100° C. or lower at a third average cooling rate of 100° C./s to 1000° C./s. In the case where the third average cooling rate is less than 100° C./s, since an excessive amount of bainite is formed, it is not possible to achieve the desired volume fractions. Therefore, the third average cooling rate is set to be 100° C./s or more. On the other hand, in the case where the third average cooling rate is more than 1000° C./s, a shrinkage cracking may occur in a steel sheet due to cooling. Therefore, the third average cooling rate is set to be 1000° C./s or less. Here, in the case of this cooling, it is preferable that water quenching be performed.
- (Tempering)
- After cooling as described above, a tempering treatment is performed. This tempering is performed in order to improve workability by softening martensite. That is, after cooling is performed as described above, in order to temper martensite, after heating has been performed to a temperature of 200° C. to 350° C., holding is performed at a tempering temperature of 200° C. to 350° C. (hereinafter, also referred to as “fourth soaking temperature”) for 120 seconds to 1200 seconds. In the case where the tempering temperature (fourth soaking temperature) is lower than 200° C., since the softening of martensite is insufficient, there is a decrease in hole expansion capability. Therefore, the fourth soaking temperature is set to be 200° C. or higher. On the other hand, the tempering temperature (fourth soaking temperature) is higher than 350° C., there is an increase in yield ratio (YR). Therefore, the fourth soaking temperature is set to be 350° C. or lower, or preferably 300° C. or lower. In addition, in the case where the holding time at the fourth soaking temperature is less than 120 seconds, since there is an insufficient improvement in the property of martensite at the fourth soaking temperature, it is not possible to expect the effect of increasing hole expansion ratio (λ). Therefore, the holding time at the fourth soaking temperature is set to be 120 seconds or more. On the other hand, in the case where the holding time at the fourth soaking temperature is more than 1200 seconds, there is a significant decrease in tensile strength due to the softening of martensite progressing excessively, and there is an increase in manufacturing costs due to an increase in reheating time. Therefore, the holding time at the fourth soaking temperature is set to be 1200 seconds or less. Here, after the holding at the above-described temperature, there is no limitation on cooling method or cooling rate.
- In addition, skin pass rolling may be performed after the annealing process. It is preferable that skin pass rolling be performed with an elongation ratio of 0.1% to 2.0%.
- Here, within the range according to embodiments of the present invention, a galvanized steel sheet may be manufactured by performing a galvanizing treatment in the annealing process, and a galvannealed steel sheet may be manufactured by performing an alloying treatment after a galvanizing treatment has been performed. Moreover, by performing an electroplating treatment on the cold-rolled steel sheet according to embodiments of the present invention, an electroplated steel sheet may be manufactured.
- Hereafter, the examples of embodiments of the present invention will be described. However, the present invention is not originally limited by the examples described below, and the present invention may be performed by appropriately making alterations within a range in accordance with the intent of the present invention. Working examples performed in such a way are all within the technical scope of the present invention.
- By preparing molten steels having the chemical compositions given in Table 1, by casting the steels in order to manufacture slabs having a thickness of 230 mm, by performing hot rolling under the conditions of a hot rolling heating temperature of 1200° C. and a finishing delivery temperature of 900° C., by performing cooling to a temperature of 650° C. at a cooling rate of 100° C./s after hot rolling had been performed, and by then performing cooling at a cooling rate of 20° C./s, hot-rolled steel sheets having a thickness of 3.2 mm were obtained and coiled at a coiling temperature of 600° C. Subsequently, by pickling the obtained hot-rolled steel sheets, and by then performing cold rolling, cold-rolled steel sheets (having a thickness of 1.4 mm) were manufactured. Subsequently, in the first annealing process, heating was performed to the first soaking temperatures given in Table 2, annealing was performed at the first soaking temperatures for the first soaking time (first holding time), cooling was the performed to the second soaking temperatures at the first average cooling rates (CR1) given in Table 2, holding was performed for the second soaking time (second holding time), and then cooling was performed to room temperature (25° C.) Subsequently, in the second annealing process, heating was performed at the average heating rates given in Table 2, holding was performed at the third soaking temperatures for the third soaking time (third holding time), cooling was then performed to the quenching start temperatures (cooling start temperatures of cooling performed at the third average cooling rates, that is, cooling stop temperatures: Tq) at the second average cooling rates (CR2) given in Table 2, cooling was then performed to room temperature (25° C.) at the third average cooling rates (CR3), and then, in the tempering process, heating was performed to the fourth soaking temperatures given in Table 2, holding was performed for the fourth soaking times (fourth holding times given in Table 2), and then cooling was performed to room temperature (25° C.)
-
TABLE 1 Steel Chemical Composition (mass %) Grade C Si Mn P S Al N Other Note A 0.20 1.45 2.21 0.01 0.002 0.03 0.002 — Example Steel B 0.18 1.56 2.19 0.01 0.001 0.03 0.003 Ti: 0.02 Example Steel C 0.21 1.81 2.31 0.01 0.001 0.03 0.003 V: 0.02 Example Steel D 0.22 1.44 1.98 0.01 0.001 0.03 0.002 Nb: 0.02 Example Steel E 0.21 1.64 2.34 0.01 0.002 0.03 0.001 B: 0.002 Example Steel F 0.22 1.31 2.21 0.01 0.001 0.03 0.001 Cr: 0.20 Example Steel G 0.20 1.38 2.14 0.01 0.001 0.03 0.002 Mo: 0.20 Example Steel H 0.19 1.84 2.01 0.01 0.001 0.03 0.002 Cu: 0.10 Example Steel I 0.21 1.65 2.21 0.01 0.001 0.03 0.003 Ni: 0.10 Example Steel J 0.19 1.54 1.89 0.01 0.002 0.03 0.002 Ca: 0.0035 Example Steel K 0.22 1.45 2.22 0.01 0.002 0.03 0.002 REM: 0.0028 Example Steel L 0.11 1.50 2.34 0.01 0.002 0.03 0.002 — Comparative Steel M 0.21 0.34 2.48 0.01 0.002 0.02 0.003 — Comparative Steel N 0.22 2.12 1.21 0.01 0.002 0.03 0.003 — Comparative Steel O 0.19 0.88 3.01 0.02 0.002 0.04 0.002 — Comparative Steel Remainder which is different from the constituent chemical elements described above: Fe and inevitable impurities Underlined portion: out of the range according to the present invention -
TABLE 2 Annealing (First) Condition Annealing (Second) Condition First First Second Second Average Third Third Fourth Fourth Soaking Holding Soaking Holding Heating Soaking Holding Soaking Holding Sample Steel Temperature Time CR1 (*1) Temperature Time Rate Temperature Time CR2 (*1) Tq (*2) CR3 (*1) Temperature Time No. Grade ° C. sec ° C./s ° C. sec ° C./s ° C. sec ° C./s ° C. ° C./s ° C. sec 1 A 850 300 10 400 600 10 800 600 5 400 880 250 600 2 B 860 600 10 400 300 10 800 600 5 400 900 250 600 3 C 860 600 10 350 600 10 800 600 5 400 900 200 600 4 D 860 300 10 350 600 5 820 500 10 400 800 250 600 5 E 850 300 10 400 300 10 800 300 10 400 840 300 300 6 F 850 200 10 420 600 10 820 120 15 420 880 250 300 7 G 850 120 10 400 300 10 790 300 10 400 800 250 300 8 H 860 300 10 400 300 15 790 300 10 380 800 250 300 9 I 860 300 20 420 300 10 800 300 10 400 890 250 300 10 J 850 120 10 400 300 10 800 300 10 400 880 250 300 11 K 850 100 5 420 600 10 820 600 10 400 900 250 300 12 L 850 300 10 400 600 10 800 300 10 400 880 250 600 13 A 750 120 10 380 600 5 820 300 10 400 880 300 600 14 A 850 3 10 400 600 10 810 300 5 380 900 250 600 15 A 850 300 1 400 600 10 800 300 10 400 900 250 600 16 A 850 300 10 200 600 10 800 300 10 450 900 250 600 17 A 850 300 10 550 300 10 810 300 10 400 880 250 600 18 A 850 300 10 400 10 10 810 300 10 400 880 250 600 19 A 850 300 10 420 300 1 810 300 10 400 890 250 600 20 A 850 300 10 400 600 10 720 300 10 400 900 250 600 21 A 850 300 10 400 600 10 810 300 1 400 800 250 600 22 A 850 300 10 350 600 10 800 300 10 200 880 250 600 23 A 860 300 10 400 300 10 800 300 10 600 890 250 600 24 A 850 300 10 400 300 10 800 300 10 400 880 100 600 25 A 850 300 10 400 300 10 800 600 10 400 900 550 600 26 A 850 300 10 400 300 10 800 300 10 400 800 250 10 27 L 850 300 10 400 300 10 800 300 10 400 900 250 300 28 M 850 300 10 400 300 10 800 300 10 400 880 250 300 29 N 850 300 10 400 300 10 800 300 10 450 880 250 600 30 O 850 300 10 400 300 10 820 300 10 400 900 250 600 Underlined portion: out of the range according to the present invention (*1) CR1, CR2, and CR3 (° C./s): respectively the first average cooling rate, the second average cooling rate, and the third average cooling rate in this order (*2) Tq (° C.): cooling stop temperature of cooling performed at the second average cooling rate (cooling start temperature of cooling performed at the third average cooling rate) - By taking a JIS No. 5 tensile test piece from the manufactured steel sheet so that a direction at a right angle to the rolling direction was the longitudinal direction (tensile direction) of the test piece, and by performing a tensile test (JIS Z 2241 (1998)), yield strength (YS), tensile strength (TS), elongation (EL), and yield ratio (YR) were determined. A steel sheet having a tensile strength (TS) of 980 MPa or more was judged as a high-strength steel sheet, a steel sheet having an elongation (EL) of 19% or more was judged as a steel sheet having a good elongation (EL), and a steel sheet having a yield ratio (YR) of 66% or less was judged as a steel sheet having the desired low yield ratio (YR).
- In addition, regarding hole expansion capability, in accordance with The Japan Iron and Steel Federation Standard (JFS T 1001 (1996)), by punching a hole having a diameter of 10 mmϕ in a sample with a clearance of 12.5%, by setting the sample on a testing machine so that the burr was on the die side, and by forming the sample with a conical punch having a point angle of 60° , hole expansion ratio (λ) was determined. A steel sheet having a λ (%) of 30% or more was judged as a steel sheet having good hole expansion capability.
- Regarding steel sheet microstructure, by using a SEM (scanning electron microscope), a TEM (transmission electron microscope), and an FE-SEM (field-emission-type scanning electron microscope), steel sheet microstructure was observed in order to identify ferrite, retained austenite, tempered martensite, and other kinds of steel microstructures.
- The volume fractions of ferrite and tempered martensite of the steel sheet were determined by polishing a cross section in the thickness direction parallel to the rolling direction of the steel sheet, by then etching the polished cross section through the use of a 3%-nital solution, by observing the etched cross section through the use of a SEM (scanning electron microscope) at magnifications of 2000 times and 5000 times, by determining the area fraction of each of the phases through the use of a point-counting method (in accordance with ASTM E562-83 (1988)), and by defining the area fraction as the volume fraction. Regarding the average crystal grain diameters of ferrite, retained austenite, and tempered martensite, since it was possible to calculate each area of the phases by inputting the steel sheet microstructure photographs, in which the crystal grains of ferrite, retained austenite, and tempered martensite had been identified in advance, into Image-Pro produced by Media Cybernetics, Inc., by calculating circle-equivalent diameters from the calculated areas, the average crystal grain diameter of each of the phases was defined as the average of the calculated circle-equivalent diameters.
- The volume fraction of retained austenite was determined by polishing the steel sheet in order to expose a surface located at ¼ of the thickness of the steel sheet and by determining the X-ray diffraction intensities of the surface. By determining the integrated intensities of X-ray diffraction of. the (200) plane, (211) plane, and (220) plane of the ferrite of iron and the (200) plane, (220) plane, and (311) plane of the austenite of iron through the use of the Ka ray of Mo as a radiation source with an acceleration voltage of 50 keV in X-ray diffractometry (apparatus: RINT-2200 produced by Rigaku Corporation), and by using the calculating formula described in “X-ray Diffraction Handbook” published by Rigaku Corporation (2000), pp. 26 and 62-64, the volume fraction of retained austenite was determined.
- In addition, the number of grains of retained austenite were determined by counting the number in the observation of a steel sheet photograph taken through the use of a SEM.
- The determined steel sheet microstructure, tensile properties, and hole expansion ratio (λ) are given in Table 3.
-
TABLE 3 Steel Sheet Microstructure Hole Number of Expansion Ferrite Retained Austenite Tempered Martensite RA Grains in Tensile Property Ratio Sample Volume Average Grain Volume Average Grain Volume Average Grain Remainder an Area of YS TS EL YR λ No. Fraction/% Diameter/μm Fraction/% Diameter/μm Fraction/% Diameter/μm Kind 1000 μm2 MPa MPa % % % Note 1 46 3 7 1 42 1 TB 15 705 1082 22 65 37 Example 2 48 3 6 1 41 1 TB 11 700 1065 21 66 36 Example 3 51 3 5 2 39 1 TB 13 688 1054 19 65 35 Example 4 48 3 7 1 40 2 TB 12 643 990 22 65 36 Example 5 41 4 6 2 48 2 TB 13 675 1025 20 66 35 Example 6 50 3 6 1 35 1 TB 15 661 1030 20 64 36 Example 7 45 3 7 2 41 2 TB 16 664 1016 19 65 37 Example 8 48 4 5 1 43 1 TB 14 664 1011 22 66 38 Example 9 50 3 6 1 39 2 TB 15 661 1003 23 66 36 Example 10 50 3 6 1 40 2 TB 13 656 1041 22 63 40 Example 11 44 3 6 1 42 2 TB 12 684 1044 22 66 35 Example 12 41 3 7 1 46 1 TB 15 674 1032 21 65 37 Example 13 38 4 6 3 49 4 TB 6 668 1033 19 65 28 Comparative Example 14 44 3 5 3 38 5 TB 8 702 1029 19 68 25 Comparative Example 15 40 4 6 4 39 4 TB 6 721 1001 19 72 27 Comparative Example 16 44 4 5 3 41 5 TB 7 709 1021 19 69 22 Comparative Example 17 46 4 6 3 38 3 TB 9 711 1009 19 70 23 Comparative Example 18 47 4 5 4 38 3 TB 5 723 1046 20 69 20 Comparative Example 19 48 6 5 2 40 3 TB 10 661 1002 19 66 22 Comparative Example 20 71 5 6 2 17 2 TB 8 578 892 24 65 34 Comparative Example 21 58 6 7 3 25 2 TB, P 11 645 964 23 67 28 Comparative Example 22 48 4 3 1 36 2 TB 4 681 1001 15 68 32 Comparative Example 23 42 3 2 2 50 4 TB 3 691 1022 14 68 33 Comparative Example 24 44 3 2 2 41 2 TB 2 633 1033 19 61 22 Comparative Example 25 43 4 2 2 40 2 TB 3 729 1039 18 70 33 Comparative Example 26 43 3 4 1 40 2 TB 5 655 1030 19 64 19 Comparative Example 27 69 4 3 2 27 2 TB 7 602 889 22 68 29 Comparative Example 28 39 4 4 2 51 2 TB 3 655 989 18 66 30 Comparative Example 29 68 5 5 2 20 2 TB, P 10 595 876 24 68 35 Comparative Example 30 35 3 6 3 63 4 TB 11 729 1088 16 67 22 Comparative Example Under lined portion: out of the range according to the present invention Microstructure: TB—tempered bainite, P—pearlite, RA—retained austenite - From the results given in Table 3, it is clarified that all the examples of the present invention had a multi-phase microstructure including ferrite having an average crystal grain diameter of 5 μm or less in an amount of 30% to 55% in terms of volume fraction, retained austenite having an average crystal grain diameter of 2 μm or less in an amount of 5% to 15% in terms of volume fraction, and tempered martensite having an average crystal grain diameter of 2 μm or less in an amount of 30% to 60% in terms of volume fraction, and, as a result, had good formability represented by an elongation (EL) of 19% or more and a hole expansion ratio (λ) of 30% or more while achieving a tensile strength of 980 MPa or more and a yield ratio (YR) of 66% or less.
- On the other hand, in the case of No. 13 where the average crystal grain diameter of retained austenite was more than 2 μm, where the average crystal grain diameter of tempered martensite was more than 2 μm, and where the number of grains of retained austenite existing in an area of 1000 gm2 was less than 10, the hole expansion ratio (λ) was less than 30%. In the case of Nos. 14 through 18 where the average crystal grain diameter of retained austenite was more than 2 μm, where the average crystal grain diameter of tempered martensite was more than 2 μm, and where the number of grains of retained austenite existing in an area of 1000 μm2 was less than 10, the yield ratio (YR) was more than 66%, and the hole expansion ratio (λ) was less than 30%.
- In addition, in the case of No. 19 where the average crystal grain diameter of ferrite was more than 5 μm and where the average crystal grain diameter of tempered martensite was more than 2 μm, the hole expansion ratio (λ) was less than 30%. In the case of No. 20 where the volume fraction of ferrite was more than 55%, where the volume fraction of tempered martensite was less than 30%, and where the number of grains of retained austenite existing in an area of 1000 μm2 was less than 10, the tensile strength (TS) was less than 980 MPa.
- In the case of No. 21 where the volume fraction of ferrite was more than 55%, where the average crystal grain diameter of ferrite was more than 5 μm, where the average crystal grain diameter of retained austenite was more than 2 μm, and where the volume fraction of tempered martensite was less than 30%, the tensile strength (TS) was less than 980 MPa, the yield ratio (YR) was more than 66%, and the hole expansion ratio (λ) was less than 30%. In the case of No. 22 where the volume fraction of retained austenite was less than 5% and where the number of grains of retained austenite existing in an area of 1000 μm2 was less than 10, the elongation (EL) was less than 19%, and the yield ratio (YR) was more than 66%.
- In the case of No. 23 where the volume fraction of retained austenite was less than 5%, where the average crystal grain diameter of tempered martensite was more than 2 μm, and where the number of grains of retained austenite existing in an area of 1000 μm2 was less than 10, the elongation (EL) was less than 19%, and the yield ratio (YR) was more than 66%.
- In the case of Nos. 24 and 26 where the volume fraction of retained austenite was less than 5% and where the number of grains of retained austenite existing in an area of 1000 μm2 was less than 10, the hole expansion ratio (λ) was less than 30%. In the case of No. 25 where the volume fraction of retained austenite was less than 5% and where the number of grains retained austenite existing in an area of 1000 μm2 was less than 10, the elongation (EL) was less than 19%, and the yield ratio (YR) was more than 66%.
- In the case of No. 27 where the C content was less than 0.15 mass %, where the volume fraction of ferrite was more than 55%, where the volume fraction of retained austenite was less than 5%, where the volume fraction of tempered martensite was less than 30%, and where the number of grains of retained austenite existing in an area of 1000 μm2 was less than 10, the tensile strength (TS) was less than 980 MPa, the yield ratio (YR) was more than 66%, and the hole expansion ratio (λ) was less than 30%. In the case of No. 28 where the Si content was less than 1.0 mass %, where the volume fraction of retained austenite was less than 5%, and where the number of grains of retained austenite existing in an area of 1000 μm2 was less than 10, the elongation (EL) was less than 19%.
- In the case of No. 29 where the Mn content was less than 1.8 mass %, where the volume fraction of ferrite was more than 55%, and where the volume fraction of tempered martensite was less than 30%, the tensile strength (TS) was less than 980 MPa, and the yield ratio (YR) was more than 66%. In the case of No. 30 where the Mn content was more than 2.5 mass %, where the average crystal grain diameter of retained austenite was more than 2 μm, where the volume fraction of tempered martensite was more than 60%, and where the average crystal grain diameter of tempered martensite was more than 2 μm, the elongation (EL) was less than 19%, the yield ratio (YR) was more than 66%, and the hole expansion ratio (λ) was less than 30%.
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| JP5321605B2 (en) * | 2011-01-27 | 2013-10-23 | Jfeスチール株式会社 | High strength cold-rolled steel sheet having excellent ductility and method for producing the same |
| JP5348268B2 (en) * | 2012-03-07 | 2013-11-20 | Jfeスチール株式会社 | High-strength cold-rolled steel sheet having excellent formability and method for producing the same |
| JP5966598B2 (en) * | 2012-05-17 | 2016-08-10 | Jfeスチール株式会社 | High yield ratio high strength cold-rolled steel sheet excellent in workability and method for producing the same |
| JP5867436B2 (en) * | 2013-03-28 | 2016-02-24 | Jfeスチール株式会社 | High strength galvannealed steel sheet and method for producing the same |
| JP5821911B2 (en) * | 2013-08-09 | 2015-11-24 | Jfeスチール株式会社 | High yield ratio high strength cold-rolled steel sheet and method for producing the same |
| JP5821912B2 (en) * | 2013-08-09 | 2015-11-24 | Jfeスチール株式会社 | High-strength cold-rolled steel sheet and manufacturing method thereof |
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2015
- 2015-12-21 WO PCT/JP2015/006347 patent/WO2016135794A1/en not_active Ceased
- 2015-12-21 US US15/553,408 patent/US20180127856A1/en not_active Abandoned
- 2015-12-21 CN CN201580076970.2A patent/CN107406930B/en active Active
- 2015-12-21 MX MX2017010910A patent/MX394289B/en unknown
- 2015-12-21 JP JP2016522827A patent/JP6048620B1/en active Active
- 2015-12-21 KR KR1020177023461A patent/KR102016432B1/en active Active
- 2015-12-21 EP EP15883094.3A patent/EP3263728B1/en active Active
Patent Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20130133792A1 (en) * | 2010-08-12 | 2013-05-30 | Jfe Steel Corporation | High-strength cold rolled sheet having excellent formability and crashworthiness and method for manufacturing the same |
| WO2014061270A1 (en) * | 2012-10-18 | 2014-04-24 | Jfeスチール株式会社 | High-strength cold-rolled steel sheet and method for manufacturing same |
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| US20180148809A1 (en) * | 2015-05-07 | 2018-05-31 | Nippon Steel & Sumitomo Metal Corporation | High-strength steel sheet and method of manufacturing the same |
| US11174529B2 (en) * | 2015-05-07 | 2021-11-16 | Nippon Steel Corporation | High-strength steel sheet and method of manufacturing the same |
| US20180207751A1 (en) * | 2015-07-28 | 2018-07-26 | Nippon Steel & Sumitomo Metal Corporation | Fillet arc welded joint and method for producing same |
| US10786873B2 (en) * | 2015-07-28 | 2020-09-29 | Nippon Steel Corporation | Fillet arc welded joint and method for producing same |
| US11208709B2 (en) | 2017-02-28 | 2021-12-28 | Jfe Steel Corporation | High-strength steel sheet and manufacturing method therefor |
| US11390930B2 (en) * | 2017-04-14 | 2022-07-19 | Jfe Steel Corporation | Steel sheet and manufacturing method therefor |
| US11549163B2 (en) | 2017-12-19 | 2023-01-10 | Arcelormittal | Cold rolled and heat treated steel sheet, method of production thereof and use of such steel to produce vehicle parts |
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| US11884990B2 (en) | 2018-02-07 | 2024-01-30 | Tata Steel Nederland Technology B.V. | High strength hot rolled or cold rolled and annealed steel and method of producing it |
| US20210002741A1 (en) * | 2018-03-30 | 2021-01-07 | Nippon Steel Corporation | High-strength steel sheet with excellent ductility and hole-expandability |
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| US20220145435A1 (en) * | 2019-03-12 | 2022-05-12 | Osaka University | Weathering steel for solid-state welding, weathering steel material for solid-state welding, solid-state welded structure and solid-state welding method |
| US12234535B2 (en) * | 2019-03-12 | 2025-02-25 | Osaka University | Weathering steel for solid-state welding, weathering steel material for solid-state welding, solid-state welded structure and solid-state welding method |
| US12180557B2 (en) | 2019-04-08 | 2024-12-31 | Nippon Steel Corporation | Cold rolled steel sheet and method for producing same |
| US12305256B2 (en) | 2019-07-29 | 2025-05-20 | Posco Co., Ltd | High-strength steel sheet and manufacturing method thereof |
| US12467108B2 (en) | 2019-07-29 | 2025-11-11 | Posco Co., Ltd | High-strength steel sheet and manufacturing method thereof |
Also Published As
| Publication number | Publication date |
|---|---|
| MX2017010910A (en) | 2017-11-24 |
| EP3263728A4 (en) | 2018-01-03 |
| MX394289B (en) | 2025-03-21 |
| JP6048620B1 (en) | 2016-12-21 |
| JPWO2016135794A1 (en) | 2017-04-27 |
| WO2016135794A1 (en) | 2016-09-01 |
| KR102016432B1 (en) | 2019-08-30 |
| EP3263728B1 (en) | 2019-09-11 |
| CN107406930B (en) | 2019-07-23 |
| KR20170107057A (en) | 2017-09-22 |
| CN107406930A (en) | 2017-11-28 |
| EP3263728A1 (en) | 2018-01-03 |
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