WO2016135794A1 - 高強度冷延鋼板およびその製造方法 - Google Patents
高強度冷延鋼板およびその製造方法 Download PDFInfo
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/14—Ferrous alloys, e.g. steel alloys containing titanium or zirconium
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- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
- C21D8/0247—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the heat treatment
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- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D6/00—Heat treatment of ferrous alloys
- C21D6/005—Heat treatment of ferrous alloys containing Mn
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- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D6/00—Heat treatment of ferrous alloys
- C21D6/008—Heat treatment of ferrous alloys containing Si
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- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
- C21D8/0221—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the working steps
- C21D8/0236—Cold rolling
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- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
- C21D8/0247—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the heat treatment
- C21D8/0263—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the heat treatment following hot rolling
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- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D9/00—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
- C21D9/46—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for sheet metals
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/001—Ferrous alloys, e.g. steel alloys containing N
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/002—Ferrous alloys, e.g. steel alloys containing In, Mg, or other elements not provided for in one single group C22C38/001 - C22C38/60
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- 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
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/02—Ferrous alloys, e.g. steel alloys containing silicon
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/04—Ferrous alloys, e.g. steel alloys containing manganese
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/06—Ferrous alloys, e.g. steel alloys containing aluminium
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/08—Ferrous alloys, e.g. steel alloys containing nickel
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/12—Ferrous alloys, e.g. steel alloys containing tungsten, tantalum, molybdenum, vanadium, or niobium
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/16—Ferrous alloys, e.g. steel alloys containing copper
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
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- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D2211/00—Microstructure comprising significant phases
- C21D2211/001—Austenite
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- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D2211/00—Microstructure comprising significant phases
- C21D2211/004—Dispersions; Precipitations
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- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D2211/00—Microstructure comprising significant phases
- C21D2211/005—Ferrite
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- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D2211/00—Microstructure comprising significant phases
- C21D2211/008—Martensite
Definitions
- a dual phase steel plate (DP steel plate) having a composite structure of ferrite and martensite is known as a high strength cold rolled steel plate having both formability and high strength.
- DP steel has a high elongation (EL), but stress is concentrated at the interface between ferrite and martensite, and cracks are likely to be generated, so there is a disadvantage that it is inferior in bendability and hole expansibility. there were.
- Patent Document 1 discloses a DP steel sheet in which the crystal grain size, volume fraction and nanohardness of ferrite are controlled. According to this DP steel sheet, the elongation (EL) is increased and bending is performed. The property can be made excellent.
- a TRIP steel plate is mentioned as a steel plate which has high strength and high elongation (EL).
- This TRIP steel sheet has a steel sheet structure containing retained austenite. When the work is deformed at a temperature equal to or higher than the martensite transformation start temperature, the retained austenite is induced and transformed into martensite by stress, and a large elongation (EL) is obtained.
- EL elongation
- this TRIP steel sheet has a drawback that cracks are generated at the interface with ferrite due to transformation of retained austenite to martensite during punching, resulting in poor hole expansibility.
- Patent Document 2 discloses a TRIP steel sheet containing bainitic ferrite in order to improve hole expandability.
- an object of the present invention is to solve these problems, and to provide a high-strength cold-rolled steel sheet having excellent elongation (EL) and hole expansion ratio ( ⁇ ) and having a low yield ratio (YR) and a method for producing the same. It is.
- the present inventors have controlled the crystal grain size and volume fraction of the steel sheet structure of ferrite, retained austenite, and tempered martensite, while maintaining a low yield ratio (YR) and high elongation (EL) and a high hole expansion ratio ( ⁇ ) was found.
- the present invention is based on the above findings.
- DP steel has a low yield ratio (YR) because movable dislocations are introduced into ferrite during martensitic transformation.
- YR yield ratio
- martensite is hard, and voids are generated at the interface, especially at the interface with soft ferrite during the punching process in the hole expanding process, and the voids are connected in the subsequent hole expanding process.
- DP steel has a low hole expansion rate ( ⁇ ).
- tempering martensite increases the hole expansion ratio ( ⁇ ), but at the same time increases the yield ratio (YR).
- Residual austenite greatly improves the elongation (EL), but, as with hard martensite, voids are generated during punching in the hole expansion process, so the hole expansion ratio ( ⁇ ) decreases. . Thus, it has been difficult to improve the balance of elongation (EL), hole expansion rate ( ⁇ ), and yield ratio (YR).
- the present inventors have found a tempering condition of tempered martensite that increases the hole expansion ratio ( ⁇ ) while ensuring a low yield ratio (YR). Furthermore, in order to suppress void connection in the hole expansion process, the average grain size of retained austenite and tempered martensite is reduced to form a steel sheet structure in which retained austenite and tempered martensite are finely dispersed. Thus, it was found that the elongation (EL) and the hole expansion rate ( ⁇ ) are improved. For that purpose, after using the reverse transformation in the second annealing process as the microstructure of bainite and martensite in the first annealing process after cold rolling, fine austenite is generated, and then transformed into bainite by cooling.
- the component composition further includes one or more selected from the group consisting of V: 0.10% or less, Nb: 0.10% or less, Ti: 0.10% or less in terms of mass%.
- the high-strength cold-rolled steel sheet according to any one of the above [3] The high-strength cold-rolled steel sheet according to [1] or [2], further containing, by mass%, B: 0.010% or less as the component composition.
- the high-strength cold-rolled steel sheet refers to a cold-rolled steel sheet having a tensile strength (TS) of 980 MPa or more.
- the average cooling rate refers to the value obtained by subtracting the cooling end temperature from the cooling start temperature divided by the cooling time.
- the average heating rate refers to the value obtained by subtracting the heating start temperature from the heating end temperature divided by the heating time.
- the tensile strength (TS) has a low yield ratio (YR) of 980 MPa or more and 66% or less, and the elongation (EL) is 19% or more.
- a high-strength cold-rolled steel sheet having a hole expansion rate ( ⁇ ) of 30% or more and having a high elongation (EL) and a high hole expansion rate ( ⁇ ) can be stably obtained.
- the high-strength cold-rolled steel sheet of the present invention is, in mass%, C: 0.15 to 0.25%, Si: 1.0 to 2.0%, Mn: 1.8 to 2.5%, P: 0 ..
- C 0.15-0.25%
- C is an element effective for increasing the strength of the steel sheet, and contributes to the generation of second-phase tempered martensite and retained austenite in the present invention. If the C content is less than 0.15%, it is difficult to make the volume fraction of tempered martensite 30% or more and the volume fraction of retained austenite 5% or more. Therefore, the tensile strength (TS) is 980 MPa or more. It becomes difficult to make. Therefore, the C content is 0.15% or more. Preferably, the C content is 0.18% or more. On the other hand, when C is contained in excess of 0.25%, the hardness difference between ferrite and tempered martensite becomes large, and a desired hole expansion rate ( ⁇ ) cannot be obtained. Therefore, the C content is 0.25% or less. Preferably, the C content is 0.23% or less.
- the main phase refers to the ferrite phase
- the second phase refers to the tempered martensite and retained austenite phases.
- the structure of the high-strength cold-rolled steel sheet of the present invention may include tempered bainite and pearlite.
- Si 1.0-2.0% Si is an element necessary for suppressing the formation of carbides during the bainite transformation in the first and second annealings and contributing to the formation of retained austenite. If the Si content is less than 1.0%, sufficient retained austenite cannot be formed. Therefore, the Si content is 1.0% or more. Preferably, the Si content is 1.3% or more. On the other hand, if Si is contained in excess of 2.0%, the ferrite volume fraction exceeds 55% and the average crystal grain size exceeds 5 ⁇ m, so that a tensile strength (TS) of 980 MPa or more cannot be obtained. The hole expansion rate ( ⁇ ) cannot be obtained. Therefore, the Si content is 2.0% or less. Preferably, the Si content is 1.8% or less.
- Mn 1.8-2.5%
- Mn is an element that contributes to increasing the strength by forming a second phase easily while strengthening the solid solution.
- Mn is an element that stabilizes austenite. If the Mn content is less than 1.8%, the volume fraction of the second phase cannot be controlled within a desired range. Therefore, the Mn content is 1.8% or more.
- Mn is contained in excess of 2.5%, the volume fraction of tempered martensite exceeds 60%, and the hardness of tempered martensite increases, and a desired hole expansion ratio ( ⁇ ) cannot be obtained. . Therefore, the Mn content is 2.5% or less.
- P 0.10% or less P contributes to high strength by solid solution strengthening.
- the P content is 0.10% or less.
- the P content is 0.05% or less.
- the S content is 0.010% or less.
- the S content is 0.005% or less.
- the extremely low S content that makes the S content less than 0.0005% increases the steelmaking cost. Therefore, the S content is preferably 0.0005% or more.
- Al 0.10% or less
- Al is an element necessary for deoxidation, but even if Al is contained in an amount exceeding 0.10%, this deoxidation effect is saturated. Therefore, the Al content is set to 0.10% or less. Preferably, the Al content is 0.08% or less. On the other hand, in order to obtain this deoxidation effect, the Al content is preferably 0.01% or more.
- N 0.010% or less N forms coarse nitrides and lowers the hole expansion rate ( ⁇ ), so the N content needs to be suppressed.
- the N content exceeds 0.010%, a desired hole expansion rate ( ⁇ ) cannot be obtained. Therefore, the N content is 0.010% or less.
- the N content is 0.006% or less.
- Inevitable impurities include, for example, Sb, Sn, Zn, Co and the like.
- the allowable ranges of these contents are Sb: 0.01% or less, Sn: 0.10% or less, Zn: 0.0. 01% or less, Co: 0.10% or less.
- Sb 0.01% or less
- Sn 0.10% or less
- Zn 0.0. 01% or less
- Co 0.10% or less.
- this invention even if it contains Ta, Mg, and Zr within the range of a normal steel composition, the effect will not be lost.
- V 0.10% or less V forms fine carbonitrides and contributes to an increase in strength. Therefore, V can be contained as necessary. In order to exhibit this effect, it is preferable to contain V 0.01% or more. On the other hand, even if a large amount of V is contained, the effect of increasing the strength exceeding 0.10% is small, and also the alloy cost is increased, so when V is contained, the V content is It is preferable to set it to 0.10% or less.
- Nb 0.10% or less Nb, like V, contributes to an increase in strength by forming fine carbonitrides, and can be contained as necessary. In order to exhibit this effect, it is preferable to make Nb content 0.005% or more. On the other hand, when Nb is contained in an amount exceeding 0.10%, the elongation (EL) is remarkably lowered. Therefore, the Nb content is preferably 0.10% or less.
- Ti 0.10% or less Ti, like V, contributes to strength increase by forming fine carbonitrides, and can be contained as necessary. In order to exhibit this effect, it is preferable to make Ti content 0.005% or more. On the other hand, if Ti is contained at a content exceeding 0.10%, the elongation (EL) is remarkably reduced, so the Ti content is preferably 0.10% or less.
- B 0.010% or less
- B is an element that improves the hardenability and contributes to high strength by facilitating the formation of the second phase, and does not significantly increase the hardness of tempered martensite while ensuring hardenability. Therefore, it can be contained as necessary. In order to exhibit this effect, it is preferable to contain B 0.0003% or more. On the other hand, even if B is contained in an amount exceeding 0.010%, the effect is saturated, so the B content is preferably 0.010% or less.
- Cr 0.50% or less Cr is an element that contributes to increasing the strength by facilitating generation of the second phase, and can be contained as necessary. In order to exhibit this effect, it is preferable to contain 0.10% or more of Cr. On the other hand, when Cr is contained in excess of 0.50%, tempered martensite is excessively generated. Therefore, when Cr is contained, the Cr content is preferably 0.50% or less.
- Mo 0.50% or less
- Mo is an element that contributes to high strength by facilitating the formation of the second phase, and further contributes to high strength by generating a part of carbide, and is contained as necessary. Can be made. In order to exhibit this effect, it is preferable to contain 0.05% or more of Mo. On the other hand, even if Mo is contained in an amount exceeding 0.50%, the effect is saturated. Therefore, when Mo is contained, the Mo content is preferably 0.50% or less.
- Cu 0.50% or less
- Cu is an element that contributes to strengthening by solid solution strengthening and also contributes to strengthening by facilitating the formation of the second phase. Can do. In order to exhibit this effect, it is preferable to contain 0.05% or more of Cu. On the other hand, even if Cu is contained in an amount exceeding 0.50%, the effect is saturated and surface defects due to Cu are likely to occur. Therefore, when Cu is contained, the Cu content is 0.50. % Or less is preferable.
- Ni 0.50% or less
- Ni is an element that contributes to strengthening by solid solution strengthening and also contributes to strengthening by facilitating the formation of the second phase. It can be included. In order to exhibit this effect, it is preferable to contain 0.05% or more of Ni. Further, when Ni is contained simultaneously with Cu, there is an effect of suppressing surface defects caused by Cu, which is effective when Cu is added. On the other hand, even if Ni is contained in an amount exceeding 0.50%, the effect is saturated. Therefore, when Ni is contained, the Ni content is preferably 0.50% or less.
- Ca 0.0050% or less Ca can be contained as necessary because it contributes to spheroidizing the shape of the sulfide and suppressing the decrease in the hole expansion rate ( ⁇ ) due to the sulfide. In order to exhibit this effect, it is preferable to contain 0.0005% or more of Ca. On the other hand, when Ca is contained in excess of 0.0050%, the effect is saturated. Therefore, when Ca is contained, the Ca content is preferably 0.0050% or less.
- REM 0.0050% or less REM, like Ca, spheroidizes the shape of the sulfide and contributes to suppressing the decrease in the hole expansion rate ( ⁇ ) due to the sulfide. it can. In order to exhibit this effect, it is preferable to contain REM 0.0005% or more. On the other hand, when REM is contained in an amount exceeding 0.0050%, the effect is saturated. Therefore, when REM is contained, the REM content is preferably 0.0050% or less.
- the high-strength cold-rolled steel sheet of the present invention has ferrite, retained austenite, and tempered martensite. Moreover, the high-strength cold-rolled steel sheet of the present invention may have tempered bainite as the balance. Ferrite has an average grain size of 5 ⁇ m or less and a volume fraction in the range of 30 to 55%. The retained austenite has an average crystal grain size of 2 ⁇ m or less and a volume fraction in the range of 5 to 15%. Tempered martensite has an average crystal grain size of 2 ⁇ m or less and a volume fraction in the range of 30 to 60%.
- 10 or more residual austenites having an average crystal grain size of 2 ⁇ m or less are present in 1000 ⁇ m 2 .
- the volume fraction described here is the volume fraction with respect to the entire steel sheet, and so on.
- the volume fraction of the above ferrite is less than 30%, the elongation (EL) decreases because there is little soft ferrite. Therefore, the volume fraction of ferrite is set to 30% or more. Preferably, the volume fraction of ferrite is 35% or more. On the other hand, if the volume fraction of ferrite exceeds 55%, it is difficult to ensure a tensile strength (TS) of 980 MPa or more. Therefore, the volume fraction of ferrite is 55% or less. Preferably, the volume fraction of ferrite is 50% or less.
- the average crystal grain size of ferrite exceeds 5 ⁇ m, voids generated on the punched end face at the time of hole expansion are liable to be connected during the hole expansion, so that a desired hole expansion ratio ( ⁇ ) cannot be obtained. Furthermore, if the average crystal grain size of ferrite exceeds 5 ⁇ m, the yield ratio (YR) cannot be made lower than the desired value. Therefore, the average crystal grain size of ferrite is 5 ⁇ m or less.
- the volume fraction of retained austenite is required in the range of 5 to 15%. If the volume fraction of retained austenite is less than 5%, the desired elongation (EL) cannot be obtained. Therefore, the volume fraction of retained austenite is 5% or more. Preferably, the volume fraction of retained austenite is 6% or more. On the other hand, when the volume fraction of retained austenite exceeds 15%, a desired hole expansion rate ( ⁇ ) cannot be obtained. Therefore, the volume fraction of retained austenite is 15% or less. Preferably, the volume fraction of retained austenite is 12% or less. In order to obtain a high hole expansion rate ( ⁇ ), the average crystal grain size of retained austenite is 2 ⁇ m or less. If the average crystal grain size of the retained austenite exceeds 2 ⁇ m, the voids are likely to be connected after the formation of voids during hole expansion. Therefore, the average crystal grain size of retained austenite is 2 ⁇ m or less.
- the volume fraction of tempered martensite is 30 to 60%. If the volume fraction of tempered martensite is less than 30%, a tensile strength of 980 MPa or more cannot be secured. On the other hand, when the volume fraction exceeds 60%, it is difficult to ensure elongation (EL).
- EL elongation
- the average crystal grain size of tempered martensite is 2 ⁇ m or less. If the average crystal grain size exceeds 2 ⁇ m, voids generated at the interface with the ferrite tend to be connected, and the desired hole expansion ratio ( ⁇ ) cannot be obtained. Therefore, the upper limit of the average crystal grain size of tempered martensite is 2 ⁇ m. To do.
- tempered bainite may be partially generated in order to obtain bainite transformation in the annealing process in order to obtain retained austenite.
- the volume fraction of the tempered bainite is not particularly limited, but is preferably 30% or less in order to ensure high elongation (EL).
- the upper limit of the number of retained austenite in 1000 ⁇ m 2 is not particularly limited. However, if the number of retained austenite in 1000 ⁇ m 2 exceeds 50, voids generated at the interface with ferrite are easily connected. One or less is preferable.
- tempered bainite and pearlite may be generated, but the above-mentioned ferrite, residual austenite, and tempered martensite have a volume fraction and average crystal grains. If the diameter and the number of retained austenite in 1000 ⁇ m 2 are satisfied, the object of the present invention can be achieved.
- the volume fraction of pearlite is preferably 5% or less.
- the volume fraction of tempered bainite is preferably 30% or less.
- the composite structure of the steel plate described above can be observed using, for example, an SEM (scanning electron microscope). Specifically, first, a plate thickness cross section parallel to the rolling direction of the steel plate is polished and then corroded with nital (alcohol solution containing nitric acid). Subsequently, a tissue photograph at a magnification of 2000 and 5000 was taken with a scanning electron microscope, and a desired region was extracted from the obtained tissue photograph data by image analysis. Image analysis software (Image-Pro ver, manufactured by Media Cybernetics, Inc.) 7) can be determined as ferrite, retained austenite, tempered martensite, or tempered bainite.
- the desired volume fraction is measured by the point count method (according to ASTM E562-83 (1988)), and the area ratio is defined as the volume fraction. be able to.
- the desired average crystal grain size can be obtained by calculating the equivalent circle diameter from a steel sheet structure photograph and averaging these values. The number of retained austenite can be measured by observing and counting the steel sheet structure photograph.
- the desired volume fraction, average crystal grain size, and number of retained austenite for ferrite, retained austenite, and tempered martensite control the steel sheet structure during the first annealing and / or the second annealing. Can be adjusted.
- a steel slab having the above component composition is subjected to hot rolling and cold rolling, and then subjected to continuous annealing on the cold-rolled steel sheet at 850 ° C.
- a first soaking temperature at a temperature of 850 ° C. or more for 30 seconds or more
- a second soaking temperature of 320 to 500 ° C., 3 ° C./s or more
- the second soaking temperature is maintained at a temperature of 320 to 500 ° C. for 30 seconds or longer, then cooled to a temperature of 100 ° C.
- the steel slab having the above component composition is heated and then subjected to rough rolling and finish rolling to obtain a hot rolled steel sheet.
- the steel slab to be used is preferably produced by a continuous casting method in order to prevent macro segregation of components, but can also be produced by an ingot-making method or a thin slab casting method.
- the preferable conditions for the hot rolling step are to first reheat to 1100 ° C. or higher without reheating after slab casting.
- the steel slab is once cooled to a temperature of 100 ° C. or lower (for example, room temperature) and then heated again.
- energy saving processes such as direct feed rolling and direct rolling, in which rolling is performed immediately after heat retention, or rolling as it is after casting, can be applied without any problem.
- the heating temperature of the slab is 1100 ° C. or higher, the rolling load can be reduced and the productivity can be improved.
- the heating temperature of the slab is 1300 ° C. or lower, the heating cost can be reduced. Therefore, the heating temperature of the slab is preferably 1100 to 1300 ° C.
- the finish rolling finish temperature is 830 ° C. or higher, so that the hot rolling is finished in the austenite single phase region, the elongation after annealing due to the non-uniform structure in the steel sheet and the increase in material anisotropy.
- the decrease in (EL) and the hole expansion rate ( ⁇ ) can be suppressed.
- the finish rolling finish temperature is preferably 830 to 950 ° C.
- the coiling temperature is not limited. However, by setting the coiling temperature to 700 ° C. or less, the formation of coarse pearlite is suppressed, and the elongation after annealing ( EL) and hole expansion rate ( ⁇ ) can be prevented from decreasing. Therefore, the winding temperature is preferably 700 ° C. or lower. More preferably, the winding temperature is 650 ° C. or lower.
- the lower limit of the coiling temperature is not particularly limited, but by setting the coiling temperature to 400 ° C. or higher, excessive formation of hard bainite and martensite can be suppressed and the cold rolling load can be reduced. Therefore, the winding temperature is preferably 400 ° C. or higher.
- the hot-rolled steel sheet can be acidified after the hot rolling step. It is preferable to remove the scale of the hot rolled sheet surface layer by pickling.
- the pickling method is not particularly limited, and may be carried out according to a conventional method.
- Cold rolling process In the method for producing a high-strength cold-rolled steel sheet of the present invention, cold rolling is performed by rolling into a cold-rolled steel sheet having a predetermined thickness after hot rolling on the steel slab or pickling on the hot-rolled steel sheet.
- a cold rolling process is not specifically limited, What is necessary is just to implement by a conventional method.
- intermediate annealing may be performed before the cold rolling process.
- the cold rolling load can be reduced by the intermediate annealing.
- the time and temperature of the intermediate annealing are not particularly limited. For example, when batch annealing is performed in a coil state, annealing is preferably performed at 450 to 800 ° C. for 10 minutes to 50 hours.
- the cold-rolled steel sheet is annealed after the cold rolling.
- recrystallization is advanced, and retained austenite and tempered martensite are formed in the steel sheet structure for high strength.
- a high hole expansion ratio ( ⁇ ) can be obtained by performing annealing twice and refining the tempered martensite and retained austenite crystal grains after annealing. it can. Untransformed austenite is transformed into bainite during cooling during the first annealing, leaving a large amount of fine retained austenite and martensite.
- the second annealing is performed to further refine the martensite crystal.
- martensite and residual austenite generated by the first annealing become nuclei of austenite generated during annealing by reverse transformation, and cooling can be performed while maintaining a fine phase during annealing. That is, by forming a steel sheet structure in which bainite, martensite, and retained austenite are homogenized to some extent by the first annealing, it is possible to perform more uniform fine dispersion by the second annealing.
- tempering is performed after excessive cooling. Thereby, it is possible to obtain a high hole expansion rate ( ⁇ ) while suppressing a decrease in elongation (EL).
- heating is performed to a temperature of 850 ° C. or higher, and the first soaking temperature is maintained at a temperature of 850 ° C. or higher for 30 seconds or longer, and then from the first soaking temperature to 320 to 500 ° C.
- a temperature of 100 ° C. or less for example, room temperature .
- heating was performed at an average heating rate of 3 to 30 ° C./s to a temperature of 750 ° C.
- the third soaking temperature was maintained at a temperature of 750 ° C. or higher for 30 seconds or longer. Cooling at a second average cooling rate of 3 ° C./s or more from a soaking temperature to a temperature of 350 to 500 ° C., cooling to a temperature of 100 ° C. or less at a third average cooling rate of 100 to 1000 ° C./s, After heating to a temperature of 350 ° C., a fourth soaking temperature is then maintained at a temperature of 200 to 350 ° C. for 120 to 1200 seconds.
- the first annealing temperature is a temperature that is in the austenite single phase region.
- the bainite after the first annealing is reduced, so that the crystal grain size of the tempered martensite and residual austenite generated the second time is increased, and the hole expansion rate ( ⁇ ) is decreased.
- the lower limit of the first soaking temperature is 850 ° C.
- the first soaking temperature is preferably set to 1000 ° C.
- the holding time (soaking time) is set to 30 seconds or more in order to progress the recrystallization and to transform part or all into austenite.
- the holding time is not particularly limited, but is preferably 600 seconds or less so that coarse carbides are not generated in the steel sheet.
- the steel sheet is cooled to a second soaking temperature of 320 to 500 ° C. at a first average cooling rate of 3 ° C./s or more in order to obtain a steel sheet structure with a high bainite. If the first average cooling rate is less than 3 ° C./s, ferrite, pearlite, and spherical cementite are excessively generated in the steel sheet structure, so the lower limit of the first average cooling rate is 3 ° C./s.
- the second soaking temperature is set to 320 to 500 ° C.
- the second soaking temperature is 350 to 450 ° C.
- ⁇ Second annealing process> Heating up to the third soaking temperature (750 ° C or higher) at an average heating rate of 3 to 30 ° C / s)
- the second annealing After annealing, the second annealing generates nuclei of ferrite and austenite formed by recrystallization by reverse transformation, and the nucleation of recrystallized ferrite is accelerated than the coarsening of the nuclei, and the grains are grown. It is possible to refine the crystal grains.
- the third soaking temperature is less than 750 ° C., austenite is generated too little, so that martensite or residual austenite having a desired volume fraction cannot be generated. Therefore, the third soaking temperature is set to 750 ° C. or higher.
- the third soaking temperature is preferably 900 ° C. or lower in order to remove the influence of the steel sheet structure generated by the first annealing by annealing in the austenite single phase region.
- the average heating rate up to the third soaking temperature 750 ° C. or higher
- the average heating rate up to the third soaking temperature 750 ° C. or higher
- the average heating rate up to the third soaking temperature 750 ° C. or higher
- the ferrite grains become coarse and a predetermined average crystal grain size cannot be obtained. Therefore, an average heating rate shall be 3 degrees C / s or more.
- the third soaking temperature is maintained at a temperature of 750 ° C. or higher for 30 seconds or longer. If the holding time at the third soaking temperature is less than 30 seconds, elements such as Mn do not concentrate sufficiently in the austenite, and the crystal grain size of untransformed austenite becomes coarse during cooling, so that the desired hole The expansion rate ( ⁇ ) cannot be obtained. Therefore, the holding time at the third soaking temperature is 30 seconds or more.
- the cooling at the second average cooling rate is set to a temperature of 350 ° C. or higher.
- the cooling at the second average cooling rate is set to a temperature of 500 ° C. or lower.
- the cooling at the second average cooling rate is preferably 370 to 450 ° C.
- Tempeing A tempering process is performed after said cooling. This tempering process is performed in order to soften martensite and improve workability. That is, after tempering, in order to temper martensite, it is heated to a temperature of 200 to 350 ° C. and then held at a tempering temperature of 200 to 350 ° C. (hereinafter also referred to as a fourth soaking temperature) for 120 to 1200 seconds. To do. When the tempering temperature (fourth soaking temperature) is less than 200 ° C., the martensite is not sufficiently softened and the hole expansibility is lowered. Therefore, the fourth soaking temperature is set to 200 ° C. or higher.
- the fourth soaking temperature is set to 350 ° C. or lower.
- the fourth soaking temperature is preferably 300 ° C. or lower.
- the holding time at the fourth soaking temperature is less than 120 seconds, the martensite modification at the fourth soaking temperature does not sufficiently occur, so an effect of improving the hole expansion rate ( ⁇ ) is expected. Can not. Therefore, the holding time at the fourth soaking temperature is 120 seconds or longer.
- the holding time at the fourth soaking temperature exceeds 1200 seconds, the tensile strength is remarkably lowered due to excessive progress of softening of martensite, and the manufacturing cost increases due to the increase in reheating time. Invite. Therefore, the holding time at the fourth soaking temperature is 1200 seconds or less. Note that the cooling method and speed after being held at the temperature are not limited.
- temper rolling may be performed after annealing.
- a preferable range of the elongation rate is 0.1 to 2.0%.
- hot dip galvanization may be performed to obtain a hot dip galvanized steel sheet, or after hot dip galvanization, an alloying treatment may be performed to obtain an alloyed hot dip galvanized steel sheet.
- the cold-rolled steel sheet may be electroplated to form an electroplated steel sheet.
- the first annealing after heating to the first soaking temperature shown in Table 2, annealing at the first soaking temperature and the first soaking time (first holding time), the first average shown in Table 2
- the sample was cooled to the second soaking temperature at the cooling rate (cooling rate 1), held at the second soaking time (second holding time), and then cooled to room temperature (25 ° C.).
- the second average cooling rate shown in Table 2 Cooling to quenching start temperature (cooling start temperature at the third average cooling rate, cooling stop temperature: Tq) at (cooling speed 2), then to room temperature (25 ° C.) at the third average cooling rate (cooling speed 3) Then, it was heated to a fourth soaking temperature shown in Table 2 as a tempering treatment, held at a fourth soaking time (fourth holding time) shown in Table 2, and cooled to room temperature (25 ° C.).
- a JIS No. 5 tensile test piece was sampled so that the direction perpendicular to the rolling direction was the longitudinal direction (tensile direction), and was subjected to a tensile test (JIS Z2241 (1998)) to yield strength (YS), tensile strength (TS), elongation (EL), and yield ratio (YR) were measured.
- a steel sheet having a tensile strength (TS) of 980 MPa or more is a high strength steel sheet
- a steel sheet having an elongation (EL) of 19% or more is a good elongation (EL)
- a yield ratio (YR) is 66% or less.
- the steel sheet had a desired low yield ratio (YR).
- the steel sheet structure was observed by SEM (scanning electron microscope), TEM (transmission electron microscope), FE-SEM (field emission scanning electron microscope)), and ferrite, residual austenite, tempered martensite, and these The types of steel structures other than were determined.
- the volume fraction of ferrite and tempered martensite in the steel sheet was 2000 times and 5000 times using SEM (scanning electron microscope) after corroding the thickness section parallel to the rolling direction of the steel sheet and corroding with 3% nital.
- the area fraction was measured by a point count method (according to ASTM E562-83 (1988)), and the area fraction was defined as the volume fraction.
- the average crystal grain size of ferrite, retained austenite, and tempered martensite is a photograph in which each ferrite, retained austenite, and martensite crystal grains are identified in advance from a steel sheet structure photograph using Image-Pro of Media Cybernetics. , The area of each phase can be calculated, the equivalent circle diameter was calculated, and the values were averaged.
- the volume fraction of retained austenite was determined by diffracting X-ray intensity on this surface after polishing the steel plate to a 1 ⁇ 4 surface in the thickness direction.
- a K ⁇ ray of Mo as a radiation source and an acceleration voltage of 50 keV
- an X-ray diffraction method (apparatus: RINT2200 manufactured by Rigaku) and a ferrite ferrite ⁇ 200 ⁇ plane, ⁇ 211 ⁇ plane, ⁇ 220 ⁇ plane, and austenite
- the integrated intensity of X-ray diffraction lines on the ⁇ 200 ⁇ plane, ⁇ 220 ⁇ plane, and ⁇ 311 ⁇ plane is measured, and using these measured values, “X-ray diffraction handbook” (2000) Rigaku Denki Co., Ltd., P. 26, 62-64, the volume fraction of retained austenite was determined.
- the number of retained austenite was measured by observing and counting steel plate photographs by SEM.
- Table 3 shows the results of the measured steel sheet structure, tensile properties, and hole expansion rate ( ⁇ ).
- ferrite having an average crystal grain size of 5 ⁇ m or less has a volume fraction of 30 to 55%
- residual austenite having an average crystal grain size of 2 ⁇ m or less has a volume fraction of 5 to 15 %
- good moldability of 19% or more (EL) and 30% or more hole expansion ratio ( ⁇ ) is obtained.
- No. No. 21 has a volume fraction exceeding 55% for ferrite, an average crystal grain size exceeding 5 ⁇ m, an average crystal grain size of retained austenite exceeding 2 ⁇ m, and a volume fraction of tempered martensite being Since it 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 ( ⁇ ) was less than 30%.
- No. No. 22 had a volume fraction of retained austenite of less than 5%, and the number of retained austenite was less than 10 in 1000 ⁇ m 2 , so that the elongation (EL) was less than 19% and the yield ratio (YR) was 66 % Exceeded.
- the volume fraction of retained austenite was less than 5%, the average crystal grain size of tempered martensite was more than 2 ⁇ m, and the number of retained austenite was less than 10 in 1000 ⁇ m 2.
- EL was less than 19% and the yield ratio (YR) was greater than 66%.
- No. Nos. 24 and 26 had a volume fraction of less than 5% for the retained austenite, and the number of retained austenite was less than 10 in 1000 ⁇ m 2 , so the hole expansion ratio ( ⁇ ) was less than 30%.
- No. 25 the volume fraction of retained austenite was less than 5%, and the number of retained austenite was less than 10 in 1000 ⁇ m 2 , so the elongation (EL) was less than 19% and the yield ratio (YR) was It exceeded 66%.
- the C content is less than 0.15% by mass
- the ferrite volume fraction is more than 55%
- the residual austenite volume fraction is less than 5%
- the tempered martensite volume fraction is Since the number of retained austenite was less than 10 in 1000 ⁇ m 2 , the tensile strength (TS) was less than 980 MPa, the yield ratio (YR) exceeded 66%, and the hole expansion ratio ( ⁇ ) was less than 30%.
- No. No. 28 has a Si content of less than 1.0% by mass, a volume fraction of retained austenite of less than 5%, and the number of retained austenite was less than 10 in 1000 ⁇ m 2 , so the elongation (EL) was It was less than 19%.
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Abstract
Description
[1]質量%で、C:0.15~0.25%、Si:1.0~2.0%、Mn:1.8~2.5%、P:0.10%以下、S:0.010%以下、Al:0.10%以下、N:0.010%以下を含有するとともに、残部がFeおよび不可避的不純物からなる成分組成を有し、
平均結晶粒径が5μm以下であるフェライトを体積分率で30~55%、平均結晶粒径が2μm以下である残留オーステナイトを体積分率で5~15%、平均結晶粒径が2μm以下である焼戻しマルテンサイトを体積分率で30~60%を含む複合組織を有し、
前記残留オーステナイトが1000μm2中に10個以上存在する高強度冷延鋼板。
[2]前記成分組成として、さらに、質量%で、V:0.10%以下、Nb:0.10%以下、Ti:0.10%以下から選択される1種以上を含有する前記[1]に記載の高強度冷延鋼板。
[3]前記成分組成として、さらに、質量%で、B:0.010%以下を含有する前記[1]または[2]に記載の高強度冷延鋼板。
[4]前記成分組成として、さらに、質量%で、Cr:0.50%以下、Mo:0.50%以下、Cu:0.50%以下、Ni:0.50%以下、Ca:0.0050%以下、REM:0.0050%以下から選択される1種以上を含有する前記[1]~[3]のいずれか1項に記載の高強度冷延鋼板。
[5]前記[1]~[4]のいずれか1つに記載の高強度冷延鋼板の製造方法であり、
鋼スラブに、熱間圧延、冷間圧延を施した後に、冷延鋼板に連続焼鈍を施すに際し、
850℃以上の温度まで加熱し、
第1均熱温度として850℃以上の温度で30秒以上保持した後、
前記第1均熱温度から320~500℃の温度まで3℃/s以上の第1平均冷却速度で冷却し、
第2均熱温度として320~500℃の温度で30秒以上保持した後、
100℃以下まで冷却し、
その後、750℃以上の温度まで3~30℃/sの平均加熱速度で加熱し、
第3均熱温度として750℃以上の温度で30秒以上保持した後、
前記第3均熱温度から350~500℃の温度まで3℃/s以上の第2平均冷却速度で冷却し、
100℃以下の温度まで100~1000℃/sの第3平均冷却速度で冷却し、
200~350℃の温度まで加熱した後、
次いで第4均熱温度として200~350℃の温度で120~1200秒保持する高強度冷延鋼板の製造方法。
Cは鋼板の高強度化に有効な元素であり、本発明における第2相の焼戻しマルテンサイト、残留オーステナイトの生成に関しても寄与する。C含有量が0.15%未満では、焼戻しマルテンサイトの体積分率を30%以上にし、残留オーステナイトの体積分率を5%以上にすることが難しいため、引張強さ(TS)を980MPa以上にすることが難しくなる。そのため、C含有量は0.15%以上とする。好ましくは、C含有量は0.18%以上である。一方、Cを0.25%超えで含有すると、フェライトと焼戻しマルテンサイトとの硬度差が大きくなり、所望の穴拡げ率(λ)が得られない。そのため、C含有量は0.25%以下とする。好ましくは、C含有量は0.23%以下である。
Siは、1回目および2回目の焼鈍におけるベイナイト変態時に炭化物生成を抑制し、残留オーステナイトの形成に寄与するために必要な元素である。Si含有量が1.0%未満であると、十分な残留オーステナイトを形成することができない。そのため、Si含有量は1.0%以上とする。好ましくは、Si含有量は1.3%以上である。一方、Siを2.0%超えで含有すると、フェライトの体積分率が55%を超え、平均結晶粒径が5μmを超えるため、980MPa以上の引張強さ(TS)を得られず、十分な穴拡げ率(λ)も得られない。そのため、Si含有量は2.0%以下とする。好ましくは、Si含有量は1.8%以下である。
Mnは固溶強化しつつ、第2相を生成しやすくすることで高強度化に寄与する元素である。また、Mnはオーステナイトを安定化させる元素である。Mn含有量が1.8%未満であると、第2相の体積分率を所望の範囲に制御できなくなる。そのため、Mn含有量は1.8%以上にする。一方、Mnを2.5%超えで含有すると、焼戻しマルテンサイトの体積分率が60%超えになり、さらには焼戻しマルテンサイトの硬度が高くなり、所望の穴拡げ率(λ)が得られない。そのため、Mn含有量は2.5%以下とする。
Pは固溶強化により高強度化に寄与するが、Pを0.10%超えで含有すると、Pの粒界への偏析が著しくなって粒界を脆化し、粒界き裂を生成し、所望の穴拡げ率(λ)が得られない。そのため、P含有量は0.10%以下とする。好ましくは、P含有量は0.05%以下である。
Sを0.010%超えで含有すると、MnSなどの硫化物が多く生成し、穴拡げ試験時の打抜き時に硫化物周辺にボイドを生成し、所望の穴拡げ率(λ)が得られない。そのため、S含有量は0.010%以下とする。好ましくは、S含有量は0.005%以下である。一方、特に下限は無いが、S含有量を0.0005%未満にする極低S化は製鋼コストが上昇する。そのため、好ましくは、S含有量は0.0005%以上である。
Alは脱酸に必要な元素であるが、Alを0.10%超えで含有しても、この脱酸効果は飽和する。そのため、Al含有量は0.10%以下とする。好ましくは、Al含有量は0.08%以下である。一方、この脱酸効果を得るために、Al含有量は0.01%以上であることが好ましい。
Nは粗大な窒化物を形成し、穴拡げ率(λ)を低下させることから、N含有量は抑える必要がある。N含有量が0.010%超えであると、所望の穴拡げ率(λ)が得られなくなる。そのため、N含有量は0.010%以下とする。好ましくは、N含有量は0.006%以下である。
Vは微細な炭窒化物を形成することで、強度上昇に寄与するため、必要に応じて含有させることができる。この効果を発揮するためには、Vを0.01%以上含有させることが好ましい。一方、多量のVを含有させても、0.10%を超えた分の強度上昇効果は小さく、そのうえ、合金コストの増加も招いてしまうため、Vを含有させる場合には、V含有量は0.10%以下とすることが好ましい。
NbもVと同様に、微細な炭窒化物を形成することで、強度上昇に寄与するため、必要に応じて含有させることができる。この効果を発揮するためには、Nb含有量を0.005%以上とすることが好ましい。一方、0.10%超えでNbを含有すると、伸び(EL)が著しく低下するため、Nb含有量は0.10%以下とすることが好ましい。
TiもVと同様に、微細な炭窒化物を形成することで、強度上昇に寄与するため、必要に応じて含有させることができる。この効果を発揮するためには、Ti含有量を0.005%以上とすることが好ましい。一方、0.10%超えでTiを含有すると、伸び(EL)が著しく低下するため、Ti含有量は0.10%以下とすることが好ましい。
Bは焼入れ性を向上させ、第2相を生成しやすくすることで高強度化に寄与し、焼入れ性を確保しつつ、焼戻しマルテンサイトの硬度を顕著に上げない元素であるため、必要に応じて含有させることができる。この効果を発揮するためには、Bを0.0003%以上含有させることが好ましい。一方、Bを0.010%超えで含有しても、その効果が飽和するため、B含有量は0.010%以下とすることが好ましい。
Crは、第2相を生成しやすくすることで高強度化に寄与する元素であり、必要に応じて含有させることができる。この効果を発揮するためには、Crを0.10%以上含有させることが好ましい。一方、Crを0.50%超えで含有させると、過剰に焼戻しマルテンサイトが生成するため、Crを含有させる場合には、Cr含有量は0.50%以下とすることが好ましい。
Moは、第2相を生成しやすくすることで高強度化に寄与し、さらに一部炭化物を生成して高強度化に寄与する元素であり、必要に応じて含有させることができる。この効果を発揮するためには、Moを0.05%以上含有させることが好ましい。一方、Moを0.50%超えで含有させても、その効果が飽和するため、Moを含有させる場合には、Mo含有量は0.50%以下とすることが好ましい。
Cuは、固溶強化により高強度化に寄与し、また、第2相を生成しやすくすることで高強度化に寄与する元素であり、必要に応じて含有させることができる。この効果を発揮するためには、Cuを0.05%以上含有させることが好ましい。一方、Cuを0.50%超えで含有させても、その効果が飽和し、またCuに起因する表面欠陥が発生しやすくなるため、Cuを含有させる場合には、Cu含有量は0.50%以下とすることが好ましい。
NiもCuと同様、固溶強化により高強度化に寄与し、また、第2相を生成しやすくすることで高強度化に寄与する元素であり、必要に応じて含有させることができる。この効果を発揮させるためには、Niを0.05%以上含有させることが好ましい。また、Cuと同時にNiを含有させると、Cu起因の表面欠陥を抑制する効果があり、Cu添加時に有効である。一方、Niを0.50%超えで含有させても、その効果が飽和するため、Niを含有させる場合には、Ni含有量は0.50%以下とすることが好ましい。
Caは、硫化物の形状を球状化し、硫化物による穴拡げ率(λ)の低下を抑制することに寄与するため、必要に応じて含有させることができる。この効果を発揮するためには、Caを0.0005%以上含有させることが好ましい。一方、Caを0.0050%超えで含有させると、その効果が飽和する。そのため、Caを含有させる場合には、Ca含有量は0.0050%以下とすることが好ましい。
REMもCaと同様に、硫化物の形状を球状化し、硫化物による穴拡げ率(λ)の低下を抑制することに寄与するため、必要に応じて含有させることができる。この効果を発揮するためには、REMを0.0005%以上含有させることが好ましい。一方、REMを0.0050%超えで含有させると、その効果が飽和する。そのため、REMを含有させる場合には、REM含有量は0.0050%以下とすることが好ましい。
熱間圧延工程では、上記成分組成を有する鋼スラブを、加熱後、粗圧延、仕上げ圧延を施し、熱延鋼板を得る。使用する鋼スラブは、成分のマクロ偏析を防止すべく連続鋳造法で製造することが好ましいが、造塊法、薄スラブ鋳造法によっても可能である。熱間圧延工程の好ましい条件は、まず、スラブ鋳造後、再加熱することなくもしくは1100℃以上に再加熱する。本発明では、鋼スラブを製造したのち、いったん100℃以下の温度(例えば、室温)まで冷却し、その後、再度加熱する従来法に加え、冷却しないで、温片のままで加熱炉に装入する、あるいは保熱をおこなった後に直ちに圧延する、あるいは鋳造後そのまま圧延する直送圧延・直接圧延などの省エネルギープロセスも問題なく適用できる。
本発明の高強度冷延鋼板の製造方法では、上記の熱間圧延工程後、熱延鋼板に酸性を実施することができる。酸洗により、熱延板表層のスケールを除去することが好ましい。酸洗方法は特に限定されず、常法に従って実施すればよい。
本発明の高強度冷延鋼板の製造方法では、上記の鋼スラブに対する熱間圧延後または熱延鋼板に対する酸洗後、所定の板厚の冷延鋼板に圧延する冷間圧延を行う。冷間圧延工程は特に限定されず常法で実施すればよい。また、冷間圧延工程前に中間焼鈍を施しても良い。中間焼鈍により、冷間圧延負荷を低減することができる。中間焼鈍の時間・温度は特に限定されるものではないが、例えばコイルの状態でバッチ焼鈍を行う場合は、450~800℃にて、10分~50時間焼鈍することが好ましい。
本発明の高強度冷延鋼板の製造方法では、上記の冷間圧延後、冷延鋼板に焼鈍を行う。焼鈍工程においては、再結晶を進行させるとともに、高強度化のため鋼板組織に残留オーステナイト、焼戻しマルテンサイトを形成させる。また、本発明の高強度冷延鋼板の製造方法では、焼鈍を2回行い、焼鈍後の焼戻しマルテンサイトや残留オーステナイトの結晶粒を微細化させることで高い穴拡げ率(λ)を得ることができる。1回目の焼鈍中の冷却途中で未変態のオーステナイトをベイナイト変態させ、微細な残留オーステナイトやマルテンサイトを多く残存させる。しかしながら、この1回目の焼鈍工程のみではマルテンサイトの結晶粒径が大きいため、所望の穴拡げ率(λ)が得られない。そこで、さらにマルテンサイトの結晶を微細化するために2回目の焼鈍を行う。これにより、1回目の焼鈍で生成したマルテンサイトや残留オーステナイトが、逆変態により焼鈍中に生成するオーステナイトの核となり、焼鈍中も微細な相を保持しつつ、冷却することが可能である。すなわち、1回目の焼鈍でベイナイトやマルテンサイト、残留オーステナイトをある程度均質化した鋼板組織にすることによって、2回目の焼鈍でさらに均一な微細分散を行うことが可能である。2回目の焼鈍では焼戻しマルテンサイトを生成するために、一旦、過度に冷却した後に焼戻し処理を行う。これにより、伸び(EL)の低下を抑制しつつ、高い穴拡げ率(λ)を得ることが可能である。
(第1均熱温度(850℃以上)まで加熱し、30秒以上保持)
1回目の焼鈍工程では、まず、第1均熱温度まで加熱する。この第1均熱温度はオーステナイト単相域である温度とする。第1均熱温度が850℃未満では、1回目の焼鈍後のベイナイトが少なくなるため、2回目に生成する焼戻しマルテンサイト、残留オーステナイトの結晶粒径が大きくなり、穴拡げ率(λ)が低下する。そのため、第1均熱温度の下限は850℃とする。好ましくは870℃以上である。また、第1均熱温度は、オーステナイトの結晶粒径が大きくならないようにするために、1000℃以下とすることが好ましい。また、上記の第1均熱温度において、再結晶の進行および一部もしくは全てをオーステナイトに変態させるため、保持時間(均熱時間)は30秒以上とする。この保持時間は、特に限定されないが、鋼板内に粗大な炭化物が生成しないようにするため、600秒以下とすることが好ましい。
1回目の焼鈍工程では、ベイナイトが多い鋼板組織にするために、3℃/s以上の第1平均冷却速度で320~500℃の第2均熱温度まで冷却する。第1平均冷却速度が3℃/s未満であると、鋼板組織中にフェライト、パーライトや球状セメンタイトが過剰に生成するため、第1平均冷却速度の下限は3℃/sとする。また、冷却停止温度(以下、第2均熱温度とも記す。)が320℃未満では冷却時に塊状マルテンサイトが過剰に生成するため、2回目の焼鈍で鋼板組織を微細均一化にすることが困難であり、所望の穴拡げ率(λ)が得られない。冷却停止温度(第2均熱温度)が500℃超えではパーライトが過剰に増加し、2回目の焼鈍で鋼板組織を微細均一化にすることが困難であり、所望の穴拡げ率(λ)が得られない。そのため、第2均熱温度は320~500℃とする。好ましくは、第2均熱温度は350~450℃である。
未変態のオーステナイトをベイナイト変態させることで、ベイナイトおよび残留オーステナイトを生成する。第2均熱温度での保持が30秒未満では、未変態のオーステナイトが多く存在することになるため、1回目の焼鈍後の鋼板組織に塊状のマルテンサイトが多く生成し、2回目の焼鈍後の鋼板組織が微細にならない。そのため、第2均熱温度での保持時間は30秒以上とする。
第2均熱温度で保持した後は、100℃以下の温度(例えば、室温)まで冷却する。これにより、ベイナイトを含んだ鋼板組織とすることができる。
(第3均熱温度(750℃以上)まで3~30℃/sの平均加熱速度で加熱)
2回目の焼鈍により、逆変態による再結晶で生成するフェライトやオーステナイトの核を生成させ、かつ再結晶のフェライトの核の生成を核の粗大化よりも早めて、粒を成長させて、焼鈍後の結晶粒を微細化させることが可能である。第3均熱温度が750℃未満では、オーステナイトの生成が少な過ぎるため、所望の体積分率のマルテンサイトや残留オーステナイトが生成出来ない。そのため、第3均熱温度は、750℃以上とする。また、第3均熱温度は、オーステナイト単相域で焼鈍することで、1回目の焼鈍で生成した鋼板組織の影響を除去するために、900℃以下とすることが好ましい。また、第3均熱温度(750℃以上)までの平均加熱速度が30℃/s超えであると再結晶が進行しにくくなる。そのため、平均加熱速度は30℃/s以下とする。また、第3均熱温度(750℃以上)までの平均加熱速度が3℃/s未満であると、フェライト粒が粗大化して所定の平均結晶粒径が得られない。そのため、平均加熱速度は3℃/s以上とする。
2回目の焼鈍では、第3均熱温度として750℃以上の温度で30秒以上保持する。第3均熱温度での保持時間が30秒未満では、Mn等の元素がオーステナイト中に十分濃化せずに、冷却中に未変態のオーステナイトの結晶粒径が粗大化するため、所望の穴拡げ率(λ)が得られない。そのため、第3均熱温度での保持時間は30秒以上とする。
残留オーステナイトを生成して、伸び(EL)を向上させるために、第3均熱温度から冷却する過程で、未変態オーステナイトへのCおよびMnの濃化、さらにベイナイト変態を促進するために3℃/s以上の第2平均冷却速度で350~500℃の温度まで冷却する。第2平均冷却速度が3℃/s未満であると鋼板組織中にパーライトや球状セメンタイトが過剰に生成する。そのため、第2平均冷却速度の下限は3℃/sとする。また、第2平均冷却速度での冷却が350℃未満までとすると、冷却時にマルテンサイトが過剰に生成し、未変態のオーステナイトが減少し、ベイナイト変態や残留オーステナイトが減少するため、所望の伸び(EL)が得られない。そのため、第2平均冷却速度での冷却は、350℃以上の温度までとする。一方、第2平均冷却速度での冷却が500℃超えまでとすると、十分に未変態オーステナイトにCやMnが濃化しないため、最終的に得られる鋼板組織に残留オーステナイトの生成が少なくなり、所望の伸び(EL)が得られない。そのため、第2平均冷却速度での冷却は、500℃以下の温度までとする。また、第2平均冷却速度での冷却は、好ましくは370~450℃までとする。
その後、微細なマルテンサイトと残留オーステナイトを生成するために100~1000℃/sの第3平均冷却速度で100℃以下の温度まで冷却する。第3平均冷却速度が100℃未満ではベイナイトが過剰に生成してしまうため、所望の体積分率が得られない。そのため、第3平均冷却速度は100℃/s以上とする。一方、第3平均冷却速度が1000℃/sより大きくなると、冷却による鋼板の収縮割れが生じるおそれがある。そのため、第3平均冷却速度は1000℃/s以下とする。なお、ここでの冷却では、水焼入れを行うことが好ましい。
上記の冷却後、焼戻し処理を行う。この焼戻し処理は、マルテンサイトを軟質化し加工性を向上させるために行う。すなわち、上記の冷却後、マルテンサイトを焼戻すため、200~350℃の温度まで加熱した後、200~350℃の焼戻し温度(以下、第4均熱温度とも記す。)で120~1200秒保持する。焼戻し温度(第4均熱温度)が200℃未満では、マルテンサイトの軟質化が不十分で穴拡げ性が低下する。そのため、第4均熱温度は、200℃以上とする。一方、焼戻し温度(第4均熱温度)が350℃を超えると、降伏比(YR)が高くなる。そのため、第4均熱温度は、350℃以下とする。第4均熱温度は、好ましくは300℃以下である。また、第4均熱温度での保持時間が120秒に満たないと、第4均熱温度におけるマルテンサイトの改質化が十分には生じないため、穴拡げ率(λ)の向上効果が期待できない。そのため、第4均熱温度での保持時間は120秒以上とする。一方、第4均熱温度における保持時間が1200秒を超えると、マルテンサイトの軟質化が過度に進行することにより引張強さが著しく低下することに加え、再加熱時間の増加により製造コストの増加を招く。そのため、第4均熱温度での保持時間は1200秒以下とする。なお、当該温度で保持した後の冷却手法および速度については限定されることはない。
Claims (5)
- 質量%で、C:0.15~0.25%、Si:1.0~2.0%、Mn:1.8~2.5%、P:0.10%以下、S:0.010%以下、Al:0.10%以下、N:0.010%以下を含有するとともに、残部がFeおよび不可避的不純物からなる成分組成を有し、
平均結晶粒径が5μm以下であるフェライトを体積分率で30~55%、平均結晶粒径が2μm以下である残留オーステナイトを体積分率で5~15%、平均結晶粒径が2μm以下である焼戻しマルテンサイトを体積分率で30~60%を含む複合組織を有し、
前記残留オーステナイトが1000μm2中に10個以上存在する高強度冷延鋼板。 - 前記成分組成として、さらに、質量%で、V:0.10%以下、Nb:0.10%以下、Ti:0.10%以下から選択される1種以上を含有する請求項1に記載の高強度冷延鋼板。
- 前記成分組成として、さらに、質量%で、B:0.010%以下を含有する請求項1または2に記載の高強度冷延鋼板。
- 前記成分組成として、さらに、質量%で、Cr:0.50%以下、Mo:0.50%以下、Cu:0.50%以下、Ni:0.50%以下、Ca:0.0050%以下、REM:0.0050%以下から選択される1種以上を含有する請求項1~3のいずれか1項に記載の高強度冷延鋼板。
- 請求項1~4のいずれか1項に記載の高強度冷延鋼板の製造方法であり、
鋼スラブに、熱間圧延、冷間圧延を施した後に、冷延鋼板に連続焼鈍を施すに際し、
850℃以上の温度まで加熱し、
第1均熱温度として850℃以上の温度で30秒以上保持した後、
前記第1均熱温度から320~500℃の温度まで3℃/s以上の第1平均冷却速度で冷却し、
第2均熱温度として320~500℃の温度で30秒以上保持した後、
100℃以下の温度まで冷却し、
その後、750℃以上の温度まで3~30℃/sの平均加熱速度で加熱し、
第3均熱温度として750℃以上の温度で30秒以上保持した後、
前記第3均熱温度から350~500℃の温度まで3℃/s以上の第2平均冷却速度で冷却し、
100℃以下の温度まで100~1000℃/sの第3平均冷却速度で冷却し、
200~350℃の温度まで加熱した後、
次いで第4均熱温度として200~350℃の温度で120~1200秒保持する高強度冷延鋼板の製造方法。
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Also Published As
Publication number | Publication date |
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JPWO2016135794A1 (ja) | 2017-04-27 |
CN107406930A (zh) | 2017-11-28 |
EP3263728A4 (en) | 2018-01-03 |
CN107406930B (zh) | 2019-07-23 |
MX2017010910A (es) | 2017-11-24 |
KR102016432B1 (ko) | 2019-08-30 |
KR20170107057A (ko) | 2017-09-22 |
EP3263728A1 (en) | 2018-01-03 |
EP3263728B1 (en) | 2019-09-11 |
US20180127856A1 (en) | 2018-05-10 |
JP6048620B1 (ja) | 2016-12-21 |
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