High-strength steel sheet and method for manufacturing same

Information

  • Patent Grant
  • 11788163
  • Patent Number
    11,788,163
  • Date Filed
    Wednesday, March 20, 2019
    5 years ago
  • Date Issued
    Tuesday, October 17, 2023
    6 months ago
Abstract
A high-strength steel sheet includes a steel structure with: ferrite being 35% to 80% and tempered martensite being greater than 5% and 20% or less in terms of area fraction; retained austenite being 8% or more in terms of volume fraction; an average grain size of: the ferrite being 6 μm or less; and the retained austenite being 3 μm or less; a value obtained by dividing an area fraction of blocky austenite by a sum of area fractions of lath-like austenite and the blocky austenite being 0.6 or more; a value obtained by dividing, by mass %, an average Mn content in the retained austenite by an average Mn content in the ferrite being 1.5 or more; and a value obtained by dividing, by mass %, an average C content in the retained austenite by an average C content in the ferrite being 3.0 or more.
Description
FIELD

The present invention relates to a high-strength steel sheet suitably used for members used in industrial fields such as automobile and electric ones and excellent in formability and a method for manufacturing same and, in particular, relates to a high-strength steel sheet having a tensile strength (TS) of 980 MPa or more and being excellent not only in ductility but also in hole expandability and a method for manufacturing same.


BACKGROUND

In recent years, from the viewpoint of conservation of the global environment, improvement in fuel efficiency of automobiles has been an important issue. Thus, increasingly, actions are taken to thin vehicle body materials by increasing the strength of the vehicle body materials and to reduce the weight of vehicle bodies. However, increasing the strength of a steel sheet, which is one of the vehicle body materials, brings about a reduction in the formability of the steel sheet, and thus there is a need to develop a steel sheet having both high strength and high ductility. As the steel sheet with high strength and high ductility, a high-strength steel sheet using deformation-induced transformation of retained austenite has been developed. This high-strength steel sheet, showing a structure having the retained austenite, is easily formed by the retained austenite during forming and is provided with high strength because of the martensitic transformation of the retained austenite after forming.


Patent Literature 1 describes a high-strength steel sheet having extremely high ductility using the deformation-induced martensitic transformation of the retained austenite with a tensile strength of 1,000 MPa or more and a total elongation (EL) of 30% or more, for example. Patent Literature 2 describes an invention achieving a high strength-ductility balance by performing a ferrite-austenite intercritical annealing using a high Mn steel. Patent Literature 3 describes an invention improving local elongation by forming a microstructure containing bainite or martensite after hot rolling in a high Mn steel, forming fine retained austenite by annealing and tempering, and, in addition, forming a structure containing tempered bainite or tempered martensite. In addition, Patent Literature 4 describes an invention forming stable retained austenite to improve total elongation by performing a ferrite-austenite intercritical annealing to concentrate Mn into untransformed austenite using a medium Mn steel.


CITATION LIST
Patent Literature



  • Patent Literature 1: Japanese Patent Application Laid-open No. S61-157625

  • Patent Literature 2: Japanese Patent Application Laid-open No. H01-259120

  • Patent Literature 3: Japanese Patent Application Laid-open No. 2003-138345

  • Patent Literature 4: Japanese Patent No. 6179677



SUMMARY
Technical Problem

The high-strength steel sheet described in Patent Literature 1 is manufactured by performing what is called austemper treatment, which austenitizes a steel sheet with C, Si, and Mn as basic components, then quenches it within a bainite transformation temperature range, and isothermally maintains it. The retained austenite is formed by enrichment of C into the austenite by this austemper treatment, in which a large amount of C addition with a content of greater than 0.3% is required in order to obtain a large amount of the retained austenite. However, when a C concentration in steel is higher, spot weldability reduces; in a C concentration greater than 0.3% in particular, the reduction is conspicuous. Thus, it is difficult to put the high-strength steel sheet described in Patent Literature 1 to practical use as an automobile steel sheet. In addition, the invention described in Patent Literature 1 mainly aims at improving the ductility of the high-strength steel sheet and does not take hole expandability and bendability into account.


In the invention described in Patent Literature 2, improvement in ductility by Mn concentration into untransformed austenite is not studied, and there is room for improvement in formability. In the invention described in Patent Literature 3, the high Mn steel is a microstructure containing a large amount of bainite or martensite tempered at a high temperature, and thus it is difficult to ensure strength. In addition, the amount of the retained austenite is limited in order to improve local elongation, and total elongation is insufficient. In the invention described in Patent Literature 4, the heat treatment time is short, the diffusion of Mn is slow, and thus it is inferred that enrichment of Mn into austenite is insufficient.


The present invention has been made in view of the above problems, and an object thereof is to provide a high-strength steel sheet having a tensile strength (TS) of 980 MPa or more and having excellent formability and a method for manufacturing the same. In the present specification, the formability means ductility and hole expandability.


Solution to Problem

To solve the above problems and to manufacture a high-strength steel sheet having excellent formability, the inventors of the present invention have conducted earnest studies from the viewpoints of a component composition of a steel sheet and a method of manufacture to find out the following. Specifically, it has been found out that a high-strength steel sheet excellent in formability such as ductility and hole expandability through the ensuring of the retained austenite stabilized with Mn can be manufactured in which 3.10% by mass or more and 4.20% by mass or less of Mn is contained, a component composition of other alloy elements such as Ti is appropriately adjusted, and a steel slab is subjected to hot rolling, then holding for more than 21,600 s within a temperature range of an Ac1 transformation temperature or more and the Ac1 transformation temperature+150° C. or less, cold rolling, then holding for 20 s or more and 900 s or less within a temperature range of the Ac1 transformation temperature or more, then cooling, then pickling treatment, holding for 20 s or more and 900 s or less within a temperature range of the Ac1 transformation temperature or more and the Ac1 transformation temperature+150° C. or less, then cooling, holding for 1,800 s to 43,200 s within a temperature range of 50° C. or more and 300° C. or less, and then cooling to bring about ferrite being 35% or more and 80% or less and tempered martensite being greater than 5% and 20% or less in terms of area fraction and retained austenite being 8% or more in terms of volume fraction, in addition, an average grain size of the ferrite being 6 μm or less, an average grain size of the retained austenite being 3 μm or less, and a value obtained by dividing an area fraction of blocky austenite by a sum of area fractions of lath-like austenite and the blocky austenite being 0.6 or more, a value obtained by dividing an average Mn content (% by mass) in the retained austenite by an average Mn content (% by mass) in the ferrite being 1.5 or more, and a value obtained by dividing an average C content (% by mass) in the retained austenite by an average C content (% by mass) in the ferrite being 3.0 or more.


The present invention has been made based on the above-mentioned knowledge, and the gist thereof is as follows.


To solve the problem and achieve the object, a high-strength steel sheet according to the present invention includes: a component composition including: by mass %, C: 0.030% to 0.250%; Si: 0.01% to 3.00%; Mn: 3.10% to 4.20%; P: 0.001% to 0.100%; S: 0.0001% to 0.0200%; N: 0.0005% to 0.0100%; Al: 0.010% to 1.200%; and balance Fe and inevitable impurities; and a steel structure with: ferrite being 35% to 80% and tempered martensite being greater than 5% and 20% or less in terms of area fraction; retained austenite being 8% or more in terms of volume fraction; an average grain size of the ferrite being 6 or less; an average grain size of the retained austenite being 3 μm or less; a value obtained by dividing an area fraction of blocky austenite by a sum of area fractions of lath-like austenite and the blocky austenite being 0.6 or more; a value obtained by dividing an average Mn content, by mass %, in the retained austenite by an average Mn content, by mass %, in the ferrite being 1.5 or more; and a value obtained by dividing an average C content, by mass %, in the retained austenite by an average C content, by mass %, in the ferrite being 3.0 or more.


Moreover, in the high-strength steel sheet according to the present invention, the high-strength steel sheet includes a diffusible hydrogen amount in steel of 0.3 ppm by mass or less.


Moreover, in the high-strength steel sheet according to the present invention, the component composition further includes: by mass %, at least one element selected from Ti: 0.005% to 0.200%; Nb: 0.005% to 0.200%; V: 0.005% to 0.500%; W:0.005% to 0.500%; B: 0.0003% to 0.0050%; Ni: 0.005% to 1.000%; Cr: 0.005% to 1.000%; Mo: 0.005% to 1.000%; Cu: 0.005% to 1.000%; Sn: 0.002% to 0.200%; Sb: 0.002% to 0.200%; Ta: 0.001% to 0.100%; Ca: 0.0005% to 0.0050%; Mg: 0.0005% to 0.0050%; Zr: 0.0005% to 0.0050%; and REM: 0.0005% to 0.0050%; and balance Fe and inevitable impurities.


Moreover, a method of manufacturing a high-strength steel sheet according to the present invention is a method including: heating a steel slab having the component composition of the high-strength steel sheet according to the present invention; hot rolling the steel slab with a finishing delivery temperature in hot rolling within a temperature range of 750° C. to 1,000° C., such that the steel slab becomes a hot rolled steel sheet; coiling up the hot rolled steel sheet within a temperature range of 300° C. to 750° C.; holding the hot rolled steel sheet for more than 21,600 s within a temperature range of an Ac1 transformation temperature to the Ac1 transformation temperature+150° C.; cold rolling the hot rolled steel sheet; holding the hot rolled steel sheet for 20 s to 900 s within a temperature range of the Ac1 transformation temperature to the Ac1 transformation temperature+150° C.; cooling the hot rolled steel sheet; holding the hot rolled steel sheet for 1,800 s to 43,200 s within a temperature range of 50° C. to 300° C.; and cooling the hot rolled steel sheet.


Moreover, a method of manufacturing a high-strength steel sheet according to the present invention is a method including: heating a steel slab having the component composition of the high-strength steel sheet according to the present invention; hot rolling the steel slab with a finishing delivery temperature in hot rolling within a temperature range of 750° C. to 1,000° C., such that the steel slab becomes a hot rolled steel sheet; coiling up the hot rolled steel sheet within a temperature range of 300° C. to 750° C.; holding the hot rolled steel sheet for more than 21,600 s within a temperature range of an Ac1 transformation temperature to the Ac1 transformation temperature+150° C.; cold rolling the hot rolled steel sheet; holding the hot rolled steel sheet for 20 s to 900 s within a temperature range of the Ac1 transformation temperature to the Ac1 transformation temperature+150° C.; cooling the hot rolled steel sheet; performing galvanization treatment on the hot rolled steel sheet; holding the hot rolled steel sheet for 1,800 s to 43,200 s within a temperature range of 50° C. to 300° C.; and cooling the hot rolled steel sheet.


Moreover, a method of manufacturing a high-strength steel sheet according to the present invention is a method including: heating a steel slab having the component composition of the high-strength steel sheet according to the present invention; hot rolling the steel slab with a finishing delivery temperature in hot rolling within a temperature range of 750° C. to 1,000° C., such that the steel slab becomes a hot rolled steel sheet; coiling up the hot rolled steel sheet within a temperature range of 300° C. to 750° C. or less; holding the hot rolled steel sheet for more than 21,600 s within a temperature range of an Ac1 transformation temperature to the Ac1 transformation temperature+150° C.; cold rolling the hot rolled steel sheet; holding the hot rolled steel sheet for 20 s to 900 s within a temperature range of the Ac1 transformation temperature to the Ac1 transformation temperature+150° C.; cooling the hot rolled steel sheet; performing galvanization treatment on the hot rolled steel sheet; performing galvannealing treatment on the hot rolled steel sheet within a temperature range of 450° C. to 600° C.; holding the hot rolled steel sheet for 1,800 s to 43,200 s within a temperature range of 50° C. to 300° C.; and cooling the hot rolled steel sheet.


Moreover, a method of manufacturing a high-strength steel sheet according to the present invention is a method including: heating a steel slab having the component composition of the high-strength steel sheet according to the present invention; hot rolling the steel slab with a finishing delivery temperature in hot rolling within a temperature range of 750° C. to 1,000°, such that the steel slab becomes a hot rolled steel sheet; coiling up the hot rolled steel sheet within a temperature range of 300° C. to 750° C.; holding the hot rolled steel sheet for more than 21,600 s within a temperature range of an Ac1 transformation temperature to the Ac1 transformation temperature+150° C.; cold rolling the hot rolled steel sheet; then holding the hot rolled steel sheet for 20 s to 900 s within a temperature range of the Ac1 transformation temperature or more; cooling the hot rolled steel sheet; performing pickling treatment on the hot rolled steel sheet; holding the hot rolled steel sheet for 20 s to 900 s within a temperature range of the Ac1 transformation temperature to the Ac1 transformation temperature+150° C.; cooling the hot rolled steel sheet; performing galvanization treatment on the hot rolled steel sheet as needed; holding the hot rolled steel sheet for 1,800 s to 43,200 s within a temperature range of 50° C. to 300° C.; and cooling the hot rolled steel sheet.


Moreover, a method of manufacturing a high-strength steel sheet according to the present invention is a method including: heating a steel slab having the component composition of the high-strength steel sheet according to the present invention; hot rolling the steel slab with a finishing delivery temperature in hot rolling within a temperature range of 750° C. to 1,000° C., such that the steel slab becomes a hot rolled steel sheet; coiling up the hot rolled steel sheet within a temperature range of 300° C. to 750° C.; holding the hot rolled steel sheet for more than 21,600 s within a temperature range of an Ac1 transformation temperature to the Ac1 transformation temperature+150° C.; cold rolling the hot rolled steel sheet; holding the hot rolled steel sheet for 20 s to 900 s within a temperature range of the Ac1 transformation temperature or more; cooling the hot rolled steel sheet; performing pickling treatment on the hot rolled steel sheet; holding the hot rolled steel sheet for 20 s to 900 s within a temperature range of the Ac1 transformation temperature to the Ac1 transformation temperature+150° C.; cooling the hot rolled steel sheet; performing galvanization treatment on the hot rolled steel sheet; performing galvannealing treatment on the hot rolled steel sheet within a temperature range of 450° C. to 600° C.; holding the hot rolled steel sheet for 1,800 s to 43,200 s within a temperature range of 50° C. to 300° C.; and cooling the hot rolled steel sheet.


Advantageous Effects of Invention

The present invention can provide a high-strength steel sheet having a tensile strength (TS) of 980 MPa or more and having excellent formability and a method for manufacturing the same.







DESCRIPTION OF EMBODIMENTS

The following describes a high-strength steel sheet and a method for manufacturing the same according to the present invention.


(1) The following describes reasons why the steel component composition is limited to the above ranges in the high-strength steel sheet according to the present invention.


[C: 0.030% or More and 0.250% or Less]


C is an element required in order to form a low-temperature transformation phase such as martensite and to increase strength. In addition, C is an element effective in increasing the stability of retained austenite and improving the ductility of the steel. When the content of C is less than 0.030%, an area fraction of ferrite is excessive, and desired strength cannot be achieved. In addition, it is difficult to ensure a sufficient volume fraction of the retained austenite, and favorable ductility cannot be achieved. On the other hand, when C is excessively added over 0.250%, an area fraction of the martensite, which is hard, is excessive. Thus, during a hole expansion test, the number of microvoids in grain boundaries of the martensite increases, and, in addition, propagation of cracks proceeds, thus reducing hole expandability. In addition, welds and heat affected parts are markedly hardened, the mechanical characteristics of the welds reduce, and thus spot weldability and arc weldability degrade. From these viewpoints, the content of C is set within a range of 0.030% or more and 0.250% or less and preferably 0.080% or more and 0.200% or less.


[Si: 0.01% or More and 3.00% or Less]


Si is effective in ensuring favorable ductility in order to improve the work hardenability of the ferrite. When the content of Si is less than 0.01%, a Si addition effect is poor, and thus the lower limit of the content of Si is set to 0.01%. However, excessive Si addition with a content of greater than 3.00% causes embrittlement of the steel and degrades ductility and hole expandability (punching). In addition, degradation in surface properties by the occurrence of red scales and the like is caused, and chemical conversion treatability and coating quality are degraded. Thus, the content of Si is set within a range of 0.01% or more and 3.00% or less and preferably 0.20% or more and 2.00% or less.


[Mn: 3.10% or More and 4.20% or Less]


Mn is an extremely important additive element in the present invention. Mn is an element stabilizing the retained austenite, is effective in ensuring favorable ductility, and, in addition, is an element increasing the strength of the steel through solid solution strengthening. Such actions are found when the content of Mn is 3.10% or more. However, excessive addition of Mn with a content of greater than 4.20% degrades chemical conversion treatability and coating quality. From these viewpoints, the content of Mn is within a range of 3.10% or more and 4.20% or less, preferably 3.20% or more and less than 4.10%, and more preferably 3.20% or more and less than 3.80%.


[P: 0.001% or More and 0.100% or Less]


P is an element having an action of solid solution strengthening and can be added in accordance with desired strength. In addition, P is an element also effective in forming a dual phase structure in order to facilitate ferrite transformation. To obtain such effects, the content of P is required to be set to 0.001% or more. On the other hand, when the content of P is greater than 0.100%, degradation in weldability is brought about, and when hot-dip galvanization is subjected to galvannealing treatment, an alloying rate is reduced, and the quality of the hot-dip galvanization is impaired. Consequently, the content of P is set within a range of 0.001% or more and 0.100% or less and preferably 0.005% or more and 0.050% or less.


[S: 0.0001% or More and 0.0200% or Less]


S segregates in grain boundaries to embrittle the steel during hot working and is present as sulfides to reduce local deformability. Thus, the upper limit of the content of S is required to be set to 0.0200% or less, preferably 0.0100% or less, and more preferably 0.0050% or less. However, due to production technical restrictions, the content of S is required to be set to 0.0001% or more. Consequently, the content of S is set within a range of 0.0001% or more and 0.0200% or less, preferably 0.0001% or more and 0.0100% or less, and more preferably 0.0001% or more and 0.0050% or less.


[N: 0.0005% or More and 0.0100% or Less]


N is an element degrading the aging resistance of the steel. When the content of N is greater than 0.0100% in particular, degradation in the aging resistance of the steel is conspicuous. Although the content of N is preferably smaller, the content of N is required to be set to 0.0005% or more due to production technical restrictions. Consequently, the content of N is set within a range of 0.0005% or more and 0.0100% or less and preferably 0.0010% or more and 0.0070% or less.


[Al: 0.001% or More and 1.200% or Less]


Al is an element effective in expanding a ferrite-austenite two-phase region and a reduction in annealing temperature dependency, that is, material quality stability. In addition, Al is an element acting as a deoxidizer and effective in the cleanliness of the steel and is preferably added in a deoxidization process. When the content of Al is less than 0.001%, its addition effect is poor, and thus the lower limit thereof is set to 0.001%. However, a large amount addition of Al with a content of greater than 1.20% increases the risk of the occurrence of steel slab cracks during continuous casting and reduces manufacturability. From these viewpoints, the content of Al is set within a range of 0.001% or more and 1.200% or less, preferably 0.020% or more and 1.000% or less, and more preferably 0.030% or more and 0.800% or less.


In addition to the above components, at least one element selected from Ti: 0.005% or more and 0.200% or less, Nb: 0.005% or more and 0.200% or less, V: 0.005% or more and 0.500% or less, W:0.005% or more and 0.500% or less, B: 0.0003% or more and 0.0050% or less, Ni: 0.005% or more and 1.000% or less, Cr: 0.005% or more and 1.000% or less, Mo: 0.005% or more and 1.000% or less, Cu: 0.005% or more and 1.000% or less, Sn: 0.002% or more and 0.200% or less, Sb: 0.002% or more and 0.200% or less, Ta: 0.001% or more and 0.1000% or less, Ca: 0.0005% or more and 0.0050% or less, Mg: 0.0005% or more and 0.0050% or less, Zr: 0.0005% or more and 0.0050% or less, and REM: 0.0005% or more and 0.0050% or less in terms of percent by mass can be contained with a residue of Fe and inevitable impurities.


[Ti: 0.005% or More and 0.200% or Less]


Ti is effective in precipitation strengthening of the steel, can reduce a hardness difference with a hard second phase (the martensite or the retained austenite) by improving the strength of the ferrite, and can ensure favorable hole expandability. The effect is achieved with a content of Ti of 0.005% or more. However, when the content of Ti is greater than 0.200%, the area fraction of the martensite, which is hard, is excessive. Thus, during a hole expansion test, the number of microvoids in grain boundaries of the martensite increases, and, in addition, propagation of cracks proceeds, thus reducing hole expandability. Consequently, when Ti is added, the content of Ti is set within a range of 0.005% or more and 0.200% or less and preferably 0.010% or more and 0.100% or less.


[Nb: 0.005% or More and 0.200% or Less, V: 0.005% or More and 0.500% or Less, and W:0.005% or More and 0.5000% or Less]


Nb, V, and W are effective in precipitation strengthening of the steel, and the effect is achieved with a content of each of them of 0.005% or more. Like the effect of Ti addition, the hardness difference with the hard second phase (the martensite or the retained austenite) can be reduced by improving the strength of the ferrite, and favorable hole expandability can be ensured. The effect is achieved with a content of each of Nb, V, and W of 0.005% or more. However, when the content of Nb is greater than 0.100%, and the content of V and W is greater than 0.5%, the area fraction of the martensite, which is hard, is excessive. Thus, during a hole expansion test, the number of microvoids in grain boundaries of the martensite increases, and, in addition, propagation of cracks proceeds, thus reducing hole expandability. Consequently, when Nb is added, the content of Nb is set within a range of 0.005% or more and 0.200% or less and preferably 0.010% or more and 0.100% or less. When V and W are added, the content of V and W is set within a range of 0.005% or more and 0.500% or less.


[B: 0.0003% or More and 0.0050% or Less]


B has an action of inhibiting formation and growth of the ferrite from austenite grain boundaries, can reduce the hardness difference with the hard second phase (the martensite or the retained austenite) by improving the strength of the ferrite, and can ensure favorable hole expandability. The effect is achieved with a content of B of 0.0003% or more. However, when the content of B is greater than 0.0050%, formability reduces. Consequently, when B is added, the content of B is set within a range of 0.0003% or more and 0.0050% or less and preferably 0.0005% or more and 0.0030% or less.


[Ni: 0.005% or More and 1.000% or Less]


Ni is an element stabilizing the retained austenite, is effective in ensuring favorable ductility, and, in addition, is an element increasing the strength of the steel through solid solution strengthening. The effect is achieved with a content of Ni of 0.005% or more. On the other hand, when Ni is added over a content of 1.000%, the area fraction of the martensite, which is hard, is excessive. Thus, during a hole expansion test, the number of microvoids in grain boundaries of the martensite increases, and, in addition, propagation of cracks proceeds, thus reducing hole expandability. Consequently, when Ni is added, the content of Ni is set within a range of 0.005% or more and 1.000% or less.


[Cr: 0.005% or More and 1.000% or Less and Mo: 0.005% or More and 1.000% or Less]


Cr and Mo have an action of improving the balance between the strength and ductility of the steel and can thus be added as needed. The effect is achieved with a content of Cr of 0.005% or more and a content of Mo of 0.005% or more. However, when they are excessively added over a content of 1.000% for Cr and a content of 1.000% for Mo, the area fraction of the martensite, which is hard, is excessive. Thus, during a hole expansion test, the number of microvoids in grain boundaries of the martensite increases, and, in addition, propagation of cracks proceeds, thus reducing hole expandability. Consequently, when these elements are added, the content of Cr is set within a range of 0.005% or more and 1.00% or less, whereas the content of Mo is set within a range of 0.005% or more and 1.000% or less.


[Cu: 0.005% or More and 1.000% or Less]


Cu is an element effective in strengthening the steel and may be used for strengthening of the steel if it is within a range set in the present invention. The effect is achieved with a content of Cu of 0.005% or more. On the other hand, when Cu is added over a content of 1.000%, the area fraction of the martensite, which is hard, is excessive. Thus, during a hole expansion test, the number of microvoids in grain boundaries of the martensite increases, and, in addition, propagation of cracks proceeds, thus reducing hole expandability. Consequently, when Cu is added, the content of Cu is set within a range of 0.005% or more and 1.000% or less.


[Sn: 0.005% or More and 0.200% or Less and Sb: 0.005% or More and 0.200% or Less]


Sn and Sb are added as needed from the viewpoint of inhibiting decarburization in a region of about a few tens of micrometers of a steel sheet surface layer occurring by the nitriding and oxidation of a steel sheet surface. Such nitriding and oxidation are inhibited, whereby a reduction in the area fraction of the martensite is inhibited on the steel sheet surface, which is effective in ensuring strength and material quality stability. On the other hand, excessive addition over a content of 0.200% for any of these elements brings about a reduction in ductility. Consequently, when Sn and Sb are added, the contents of Sn and Sb are each set within a range of 0.002% or more and 0.200% or less.


[Ta: 0.001% or More and 0.100% or Less]


Like Ti and Nb, Ta forms alloy carbides and alloy carbonitrides to contribute to strengthening of the steel. In addition, it is considered that Ta is partially solid dissolved in Nb carbides and Nb carbonitrides to form composite precipitates such as (Nb, Ta) and (C, N) and thus produces an effect of significantly inhibiting coarsening of the precipitates and stabilizing contribution to the strength of the steel by precipitation strengthening. Thus, Ta is preferably contained. The effect of precipitate stabilization described above is achieved by setting the content of Ta to 0.001% or more. On the other hand, excessive addition of Ta saturates the precipitate stabilization effect and besides increases alloy costs. Consequently, when Ta is added, the content of Ta is set within a range of 0.001% or more and 0.100% or less.


[Ca: 0.0005% or More and 0.0050% or Less, Mg: 0.0005% or More and 0.0050% or Less, Zr: 0.0005% or More and 0.0050% or Less, and REM: 0.0005% or More and 0.0050% or Less]


Ca, Mg, Zr, and REM are elements effective in making the shape of sulfides spherical and remedying an adverse effect of the sulfides on hole expandability. To achieve this effect, they each require a content of 0.0005% or more. However, excessive addition with a content of greater than 0.0050% for each of them brings about an increase in inclusions and the like and causes surface and internal defects and the like. Consequently, when Ca, Mg, Zr, and REM are added, the contents of them are each set within a range of 0.0005% or more and 0.0050% or less.


(2) The following describes a microstructure of the high-strength steel sheet according to the present invention.


[Area Fraction of Ferrite: 35% or More and 80% or Less]


To ensure sufficient ductility of the steel, the area fraction of the ferrite is required to be set to 35% or more. To ensure a strength of 980 MPa or more, the area fraction of the ferrite, which is soft, is required to be set to 80% or less. The area fraction of the ferrite is preferably set within a range of 40% or more and 75% or less.


[Area Fraction of Tempered Martensite: Greater than 5% and 20% or Less]


Tempered martensite is required in order to ensure favorable hole expandability. To achieve a TS of 980 MPa or more, an area fraction of the tempered martensite is required be set to 20% or less. The area fraction of the tempered martensite is set within a range of preferably greater than 5% and 18% or less and more preferably greater than 10% and 18% or less. The area fractions of the ferrite and the tempered martensite were determined by polishing a sheet thickness section (an L section) parallel to a rolling direction of the steel sheet, then etching the section with 3 vol % nital, observing a sheet thickness ¼ position (a position corresponding to ¼ of a sheet thickness from the steel sheet surface in a depth direction) for ten fields of view with a 2,000-fold magnification using a scanning electron microscope (SEM), calculating area fractions of the respective structures (the ferrite and the tempered martensite) for 10 fields of view using Image-Pro of Media Cybernetics, Inc. using obtained structure images, and averaging those values. In the structure images, the ferrite shows a grey structure (an underlying structure), whereas the tempered martensite shows a structure having a grey internal structure inside white martensite.


[Volume Fraction of Retained Austenite: 8% or More]


To ensure sufficient ductility of the steel, a volume fraction of the retained austenite is required to be set to 8% or more. The volume fraction of the retained austenite is preferably within a range of 12% or more. The volume fraction of the retained austenite was determined by, for a plane obtained by polishing the steel sheet to a plane 0.1 mm distant from the sheet thickness ¼ position and then polishing it by additional 0.1 mm by chemical polishing, measuring respective integral intensity ratios of diffraction peaks of the (200), (220), and (311) planes of fcc iron and the (200), (211), and (220) planes of bcc iron using the CoKα line with an X-ray diffraction apparatus, and averaging the obtained nine integral intensity ratios.


[Average Grain Size of Ferrite: 6 μm or Less]


Fining grains of the ferrite contributes to improvement in TS. Thus, to ensure a desired TS, an average grain size of the ferrite is required to be set to 6 μm or less. The average grain size of the ferrite is preferably set within a range of 5 μm or less.


[Average Grain Size of Retained Austenite: 3 or Less]


Fining grains of the retained austenite contributes to improvement in the ductility and hole expandability of the steel. Thus, to ensure favorable ductility and hole expandability, an average grain size of the retained austenite is required to be set to 3 μm or less. The average grain size of the retained austenite is preferably set within a range of 2.5 μm or less. The average grain sizes of the ferrite, the tempered martensite, and the retained austenite were determined by determining respective areas of ferrite grains, tempered martensite grains, and retained austenite grains, calculating circle-equivalent diameters, and averaging those values using Image-Pro described above.


[Value Obtained by Dividing Area Fraction of Blocky Austenite by Sum of Area Fractions of Lath-Like Austenite and Blocky Austenite of 0.6 or More]


An area fraction of blocky austenite contributes to improvement in the hole expandability of the steel. Thus, to ensure favorable hole expandability, a value obtained by dividing the area fraction of the blocky austenite by the sum of area fractions of lath-like austenite and the blocky austenite is required to be set within a range of 0.6 or more. The value obtained by dividing the area fraction of the blocky austenite by the sum of area fractions of lath-like austenite and the blocky austenite is preferably set within a range of 0.8 or more. The blocky austenite referred to here is one with a major axis-to-minor axis aspect ratio of less than 2.0, whereas lath-like austenite indicates one with a major axis-to-minor axis aspect ratio of 2.0 or more. An aspect ratio of the retained austenite was calculated by drawing an oval circumscribing a retained austenite grain and dividing its major axis length by its minor axis length using Photoshop elements 13.


[Value Obtained by Dividing Average Mn Content (% by Mass) in Retained Austenite by Average Mn Content (% by Mass) in Ferrite: 1.5 or More]


That a value obtained by dividing an average Mn content (% by mass) in the retained austenite by an average Mn content (% by mass) in the ferrite is 1.5 or more is an extremely important constituent matter in the present invention. To ensure favorable ductility, the volume fraction of the stable retained austenite in which Mn is concentrated is required to be high. The value obtained by dividing an average Mn content (% by mass) in the retained austenite by an average Mn content (% by mass) in the ferrite is preferably within a range of 2.0 or more. The average Mn content in the retained austenite was determined by quantifying Mn distribution states to the respective phases of a section in the rolling direction at the sheet thickness ¼ position and through averages of quantity analysis results of 30 retained austenite grains and 30 ferrite grains using an electron probe micro analyzer (EPMA).


[Value Obtained by Dividing Average C Content (% by Mass) in Retained Austenite by Average C Content (% by Mass) in Ferrite: 3.0 or More]


That a value obtained by dividing an average C content (% by mass) in the retained austenite by an average C content (% by mass) in the ferrite is 3.0 or more is an extremely important constituent matter in the present invention. To ensure favorable ductility, the volume fraction of the stable retained austenite in which C is concentrated is required to be high. The value obtained by dividing an average C content (% by mass) in the retained austenite by an average C content (% by mass) in the ferrite is preferably set within a range of 5.0 or more. The average C content in the retained austenite was determined by quantifying C distribution states to the respective phases of a section in the rolling direction at the sheet thickness ¼ position and through averages of quantity analysis results of 30 retained austenite grains and 30 ferrite grains using EPMA.


[Diffusible Hydrogen Amount in Steel: 0.3 ppm by Mass or Less]


That a diffusible hydrogen amount in steel is 0.3 ppm by mass or less is an important constituent matter in the present invention. To ensure favorable hole expandability, the diffusible hydrogen amount in steel is required to be set to 0.3 ppm by mass or less. The diffusible hydrogen amount in steel is preferably within a range of 0.2 ppm by mass or less. A test piece with a length of 30 mm and a width of 5 mm was collected from an annealed sheet, a plated layer was polished to be removed, and then a diffusible hydrogen amount in the steel and a discharge peak of the diffusible hydrogen were measured. The discharge peak was measured by thermal desorption spectrometry (TDS), in which a temperature rising rate was set to 200° C./hr. Hydrogen detected at 300° C. or less was determined to be the diffusible hydrogen.


Even when the microscopic structure of the high-strength steel sheet according to the present invention contains fresh martensite, bainite, tempered bainite, pearlite, and carbides such as cementite within a range of 10% or less in terms of area fraction apart from the ferrite, the tempered martensite, and the retained austenite, the effects of the present invention are not impaired.


(3) The following describes manufacturing conditions of the high-strength steel sheet according to the present invention.


[Heating Temperature of Steel Slab]


A heating temperature of a steel slab, which is not limited to a particular temperature, is preferably set within a range of 1,100° C. or more and 1,300° C. or less. Precipitates present in a heating stage of the steel slab will be present as coarse precipitates within a steel sheet to be finally obtained and do not contribute to the strength of the steel, and thus Ti- and Nb-based precipitates precipitated during casting are required to be redissolved. When the heating temperature of the steel slab is less than 1,100° C., sufficient solid dissolving of carbides is difficult, causing a problem in that the risk of the occurrence of troubles during hot rolling caused by an increase in a rolling load increases or the like. Thus, the heating temperature of the steel slab is required to be set to 1,100° C. or more. In addition, also from the viewpoint of removing defects such as bubbles and segregation on a slab surface layer, reducing cracks and irregularities on the steel sheet surface, and achieving a smooth steel sheet surface, the heating temperature of the steel slab is required to be set to 1,100° C. or more. On the other hand, when the heating temperature of the steel slab is higher than 1,300° C., scale loss increases along with an increase in the amount of oxidation, and thus the heating temperature of the steel slab is required to be set to 1,300° C. or less. The heating temperature of the steel slab is more preferably set within a temperature range of 1,150° C. or more and 1,250° C. or less.


Although the steel slab is preferably manufactured by continuous casting in order to prevent macrosegregation, it can also be manufactured by ingot making, thin slab casting, or the like. In addition to a conventional method in which a steel slab is manufactured, then once cooled to room temperature, and then reheated, an energy-saving process such as direct feed rolling or direct rolling, which charges the steel slab into a heating furnace without being cooled to room temperature while remaining a hot slab or rolls the steel slab immediately after performing slight heat retention, can also be used without any problem. The steel slab is formed into a sheet bar by coarse rolling on normal conditions; when the heating temperature is set to a lower temperature, the sheet bar is preferably heated using a bar heater or the like before finishing rolling from the viewpoint of preventing troubles during hot rolling.


[Finishing Delivery Temperature in Hot Rolling of Hot Rolling: 750° C. or More and 1,000° C. or Less]


The steel slab after heating is hot rolled by coarse rolling and finishing rolling to be a hot rolled steel sheet. In this process, when a finishing delivery temperature in hot rolling is higher than 1,000° C., the production of oxides (scales) rapidly increases, the interface between base iron and the oxides roughens, and thus surface quality after pickling and cold rolling tends to degrade. When residues of hot rolling scales or the like are partially present after the pickling, the ductility and hole expandability of the steel are adversely affected. In addition, grain size may excessively be coarse, and pressed article surface roughness may occur during the working. On the other hand, when the finishing delivery temperature in hot rolling is less than 750° C., the rolling load increases to increase a rolling burden. In addition, a rolling reduction ratio in a state in which austenite is non-recrystallized increases, the average grain size of the ferrite coarsens, in addition, an abnormal texture develops, in-plane anisotropy in a final product is conspicuous, and not only the uniformity of material quality (material quality stability) is impaired, but also it is difficult to ensure the strength and ductility of the steel. Consequently, the finishing delivery temperature in hot rolling of hot rolling is set within a temperature range of 750° C. or more and 1,000° C. or less and preferably 800° C. or more and 950° C. or less.


[Average Coiling Temperature in Coil after Hot Rolling: 300° C. or More and 750° C. or Less]


When an average coiling temperature in coil after the hot rolling is higher than 750° C., the grain size of ferrite of a hot rolled steel sheet structure increases, making it difficult to ensure desired strength and ductility of a final annealed sheet. On the other hand, when the average coiling temperature in coil after the hot rolling is less than 300° C., hot rolled steel sheet strength increases, which increases a rolling load in cold rolling or causes faulty sheet shape, and thus productivity is reduced. Consequently, the average coiling temperature in coil after the hot rolling is set within a temperature range of 300° C. or more and 750° C. or less and preferably 400° C. or more and 650° C. or less. During the hot rolling, coarsely rolled steel sheets may be joined together to continuously perform the finishing rolling. The coarsely rolled steel sheet may once be coiled. To reduce the rolling load during the hot rolling, part or the whole of the finishing rolling may be lubricating rolling. Performing the lubricating rolling is effective also from the viewpoint of making steel sheet shape and material quality uniform. A friction coefficient during the lubricating rolling is preferably set within a range of 0.10 or more and 0.25 or less. The thus manufactured hot rolled steel sheet is subjected to pickling. The pickling can remove oxides on the steel sheet surface and is thus important for ensuring favorable chemical conversion treatability and coating quality of a high-strength steel sheet as a final product. The pickling may be performed once, or the pickling may be performed separately a plurality of times.


[Holding for More than 21,600 s within Temperature Range of Ac1 Transformation Temperature or More and Ac1 Transformation Temperature+150° C. or Less]


That the coil after the hot rolling is subjected to holding for more than 21,600 s within a temperature range of an Ac1 transformation temperature or more and the Ac1 transformation temperature+150° C. or less is an extremely important invention constituent matter in the present invention. In the case of holding within a temperature range of less than the Ac1 transformation temperature, within a temperature range of higher than the Ac1 transformation temperature+150° C., and for less than 21600 s, concentration of Mn into the austenite does not sufficiently proceed, making it difficult to ensure a sufficient volume fraction of the retained austenite after final annealing, and the ductility of the steel reduces. The holding time is preferably 129,600 s or less. In the case of holding for over 129,600 s, concentration of Mn into the austenite is saturated, and not only an effect allowance for ductility after the final annealing reduces, but also cost may increase. The method of heat treatment may be any method of annealing of continuous annealing and batch annealing. After the heat treatment, the steel is cooled to room temperature; the method of cooling and the rate of cooling are not fixed to particular ones, and any cooling may be used including furnace cooling and air cooling in the batch annealing and gas jet cooling, mist cooling, and water cooling in the continuous annealing. When pickling treatment is performed, a normal method may be used.


[Holding for 20 s or More and 900 s or Less within Temperature Range of Ac1 Transformation Temperature or More]


After the cold rolling, annealing treatment holding for 20 s or more and 900 s or less within a temperature range of the Ac1 transformation temperature or more is performed as needed. In the case of within a temperature range of less than the Ac1 transformation temperature, holding for less than 20 s, and holding for over 900 s, concentration of Mn into the austenite does not sufficiently proceed, making it difficult to ensure a sufficient volume fraction of the retained austenite after the final annealing, and the ductility of the steel reduces.


[Holding for 20 s or More and 900 s or Less within Temperature Range of Ac1 Transformation Temperature or More and Ac1 Transformation Temperature+150° C. or Less]


Holding for 20 s or more and 900 s or less within a temperature range of the Ac1 transformation temperature or more and the Ac1 transformation temperature+150° C. or less is an extremely important invention constituent matter in the present invention. In the case of holding within a temperature range of less than the Ac1 transformation temperature and for less than 20 s, carbides formed during temperature rising remain undissolved, making it difficult to ensure a sufficient volume fraction of the retained austenite, and the ductility of the steel reduces. In addition, the area fraction of the ferrite increases, making it difficult to ensure strength. On the other hand, in the case of holding within a temperature range of higher than the Ac1 transformation temperature+150° C. and for over 900 s, concentration of Mn into the austenite does not sufficiently proceed, making it unable to obtain a sufficient volume fraction of the retained austenite for the ensuring of ductility. In addition, the area fraction of the martensite increases, strength increases, making it difficult to ensure ductility. The upper limit of the temperature range is preferably the Ac1 transformation temperature+100° C. or less. When the annealing treatment holding for 20 s or more and 900 s or less within a temperature range of the Ac1 transformation temperature or more is performed, this annealing treatment holding for 20 s or more and 900 s or less within a temperature range of the Ac1 transformation temperature or more and the Ac1 transformation temperature+150° C. or less is performed thereafter.


[Performing Coating Treatment]


When hot-dip galvanization treatment is performed, the steel sheet that has been subjected to the annealing treatment holding for 20 s or more and 900 s or less within a temperature range of the Ac1 transformation temperature or more and the Ac1 transformation temperature+150° C. or less is immersed in a hot-dip galvanization bath within a temperature range of 440° C. or more and 500° C. or less to perform the hot-dip galvanization treatment, and then a coating adhesion amount is adjusted by gas wiping or the like. As the hot-dip galvanization bath, a hot-dip galvanization bath with an Al amount of within a range of 0.08% or more and 0.30% or less is preferably used. When galvannealing treatment for hot-dip galvanization is performed, after the hot-dip galvanization treatment, the galvannealing treatment for hot-dip galvanization is performed within a temperature range of 450° C. or more and 600° C. or less. When the galvannealing treatment is performed at a temperature higher than 600° C., untransformed austenite transforms into pearlite, thus a desired volume fraction of the retained austenite cannot be ensured, and thus the ductility of the steel may reduce. Consequently, when the galvannealing treatment for hot-dip galvanization is performed, the galvannealing treatment for hot-dip galvanization is preferably performed within a temperature range of 450° C. or more and 600° C. or less. Other conditions of the method of manufacture are not limited to particular ones; from the viewpoint of productivity, the annealing treatment is preferably performed with continuous annealing equipment. A series of pieces of treatment including annealing, hot-dip galvanization, and galvannealing treatment for galvanization are preferably performed with a continuous galvanizing line (CGL) as a hot-dip galvanization line.


When a high-strength hot-dip galvanized steel sheet and a high-strength hot-dip galvannealed steel sheet are manufactured, after the cold rolling, after the annealing treatment holding for 20 s or more and 900 s or less within a temperature range of the Ac1 transformation temperature or more, the annealing treatment holding for 20 s or more and 900 s or less within a temperature range of the Ac1 transformation temperature or more and the Ac1 transformation temperature+150° C. or less is performed, and pickling treatment is preferably performed between the two pieces of annealing treatment. Thus, finally favorable coating quality is obtained. This is because oxides are inhibited from being present on the surface immediately before the coating treatment, and thus uncoating by the oxides is inhibited. More specifically, this is because easily oxidizable elements (such as Mn, Cr, and Si) form oxides to be concentrated on the steel sheet surface during the heat treatment, and thus an easily oxidizable element depletion layer is formed on the steel sheet surface (immediately below the oxides) after the heat treatment, and when the oxides by the easily oxidizable elements are removed by the subsequent pickling treatment, the easily oxidizable element depletion layer appears on the steel sheet surface, and surface oxidation of the easily oxidizable elements is inhibited during the subsequent heat treatment. Also for a cold rolled steel sheet without coating treatment, after the cold rolling, the annealing treatment holding for 20 s or more and 900 s or less within a temperature range of the Ac1 transformation temperature or more and the Ac1 transformation temperature+150° C. or less may be performed after the annealing treatment holding for 20 s or more and 900 s or less within a temperature range of the Ac1 transformation temperature or more. In that process, pickling treatment may be performed between the two pieces of annealing treatment.


[Holding for 1,800 s or More and 43,200 s or Less within Temperature Range of 50° C. or More and 300° C. or Less]


That holding for 1,800 s or more and 43,200 s or less within a temperature range of 50° C. or more and 300° C. or less as the final heat treatment is an important invention constituent matter in the present invention. In the case of holding within a temperature range of less than 50° C. or for less than 1,800 s, a sufficient volume fraction of the tempered martensite cannot be obtained, in addition, intra-steel diffusive hydrogen is not discharged from the steel sheet, and thus hole expandability reduces. On the other hand, in the case of holding within a temperature range of over 300° C. or for over 43,200 s, owing to decomposition of the retained austenite, a sufficient volume fraction of the retained austenite cannot be obtained, and the ductility of the steel reduces. When the above-mentioned coating treatment is performed, after the coating treatment, the heat treatment holding for 1,800 s or more and 43,200 s or less within a temperature range of 50° C. or more and 300° C. or less is performed.


“The high-strength steel sheet” and “the high-strength hot-dip galvanized steel sheet” may be subjected to skin pass rolling for the purpose of shape correction and surface roughness adjustment. A rolling reduction ratio of the skin pass rolling is preferably set within a range of 0.1% or more and 2.0% or less. In the case of a rolling reduction ratio of less than 0.1%, the effect is small, and control is difficult, and thus this is the lower limit of a favorable range. When the rolling reduction ratio is greater than 2.0%, productivity significantly reduces, and thus this is set to the upper limit of the favorable range. The skin pass rolling may be performed online or performed offline. The skin pass rolling with a target rolling reduction ratio may be performed once or may be performed separately a plurality of times. Various kinds of coating treatment such as resin or oil-and-fat coating can be performed.


EXAMPLES

Steels having component compositions listed in Table 1 with a residue of Fe and inevitable impurities were melted with a converter to make slabs by continuous casting. The obtained slabs were reheated up to 1,250° C. and were then subjected to, on conditions listed in Table 2, hot rolling, annealing at the Ac1 transformation temperature or more, cold rolling, annealing holding for 20 s or more and 900 s or less within a temperature range of the Ac1 transformation temperature or more as needed, annealing within a temperature range of the Ac1 transformation temperature or more and the Ac1 transformation temperature+150° C. or less to obtain high-strength cold rolled steel sheets (CR) and, in addition, were subjected to hot-dip galvanization treatment as needed to obtain hot-dip galvanized steel sheets (GI) and hot-dip galvannealed steel sheets (GA). When the hot-dip galvanization treatment was performed, and the annealing treatment holding for 20 s or more and 900 s or less within a temperature range of the Ac1 transformation temperature or more and the annealing treatment within a temperature range of the Ac1 transformation temperature or more and the Ac1 transformation temperature+150° C. or less were performed, pickling treatment was performed between the two pieces of annealing treatment. As hot-dip galvanization baths, an Al: 0.19% by mass-containing zinc bath was used for the hot-dip galvanized steel sheets (GI), whereas an Al: 0.14% by mass-containing zinc bath was used for the hot-dip galvannealed steel sheets (GA), with a bath temperature of 465° C. A coating adhesion amount was set to 45 g/m2 per one side (double-sided coating), and for GA, an Fe concentration in a coating layer was adjusted so as to be within a range of 9% by mass or more and 12% by mass or less. Subsequently, as the final heat treatment, holding for 1,800 s or more and 43,200 s or less within a temperature range of 50° C. or more and 300° C. or less was performed. The sectional microscopic structure, tensile characteristics, hole expandability, chemical conversion treatability, and coatability of the obtained steel sheets were evaluated. Table 3 lists evaluation results.










TABLE 1







Steel
Component composition (% by mass)





















type
C
Si
Mn
P
S
N
Al
Ti
Nb
V
W
B
Ni
Cr





A
0.158
0.49
3.49
0.022
0.0027
0.0041
0.031
0.030








B
0.181
0.77
3.02
0.021
0.0031
0.0033
0.048
0.042








C
0.161
1.32
3.62
0.022
0.0024
0.0043
0.048
0.043








D
0.242
1.01
3.09
0.023
0.0032
0.0037
0.036









E
0.036
0.85
4.03
0.029
0.0031
0.0042
0.049









F
0.170
2.83
3.75
0.025
0.0033
0.0031
0.036









G
0.176
0.04
3.30
0.025
0.0034
0.0037
0.039
0.189








H
0.212
0.26
4.18
0.025
0.0025
0.0044
0.040









I
0.160
1.88
3.12
0.030
0.0030
0.0035
0.045









J

0.011

2.10
3.84
0.029
0.0031
0.0036
0.032









K
0.204

4.49

3.51
0.025
0.0021
0.0043
0.033









L
0.150
1.35

6.33

0.028
0.0023
0.0041
0.034









M
0.202
1.11
3.54
0.030
0.0023
0.0039
0.219
0.062








N
0.167
1.20
3.79
0.028
0.0032
0.0042
0.048

0.002









O
0.181
0.91
3.49
0.025
0.0023
0.004 
0.048
0.039
0.043







P
0.199
1.12
3.66
0.021
0.0031
0.0032
0.048


0.035






Q
0.125
0.80
4.11
0.029
0.0032
0.0044
0.044



0.018





R
0.115
0.33
3.99
0.022
0.0025
0.0034
0.048
0.057



0.0014




S
0.133
0.71
3.69
0.027
0.0031
0.0036
0.033
0.026




0.299



T
0.102
0.55
3.38
0.022
0.0024
0.0043
0.041
0.032





0.345


U
0.099
1.44
3.12
0.027
0.0033
0.0043
0.032
0.027








V
0.085
0.55
3.64
0.021
0.0029
0.0031
0.040









W
0.122
0.62
3.21
0.028
0.0021
0.0035
0.035
0.056








X
0.159
0.54
3.25
0.028
0.0033
0.0041
0.034
0.047








Y
0.176
0.69
3.64
0.022
0.0024
0.0042
0.031









Z
0.203
0.33
3.18
0.023
0.0029
0.0036
0.030

0.032







AA
0.011
0.50
3.75
0.021
0.0024
0.0044
0.050

0.038







AB
0.174
0.99
4.01
0.025
0.0028
0.0042
0.042









AC
0.189
0.05
3.78
0.027
0.0022
0.0031
0.037









AD
0.241
1.02
3.11
0.024
0.0030
0.0036
0.040
0.010








AE
0.073
0.25
4.12
0.023
0.0021
0.0042
0.048

























Ac3 trans-















Ac1 trans-
formation















formation
temper-
















Steel
Component composition (% by mass)
temperature
ature
























type
Mo
Cu
Sn
Sb
Ta
Ca
Mg
Zr
REM
(° C.)
(° C.)
Remarks







A









656
765
Example steel




B









672
794
Example steel




C









662
806
Example steel




D









672
770
Example steel




E









647
799
Example steel




F









674
848
Example steel




G









656
811
Example steel




H









633
711
Example steel




I









682
829
Example steel




J









666
874
Comparative
















steel




K









699
922
Comparative
















steel




L









586
709
Comparative
















steel




M









661
831
Example steel




N









655
778
Comparative
















steel




O









660
785
Example steel




P









658
770
Example steel




Q









643
760
Example steel




R









641
769
Example steel




S









649
770
Example steel




T









665
781
Example steel




U
0.250








679
843
Example steel




V

0.274







654
769
Example steel




W


0.006






666
800
Example steel




X



0.008





663
781
Example steel




Y




0.005




654
753
Example steel




Z


0.007






662
744
Example steel




AA




0.008




651
808
Example steel




AB





0.0023



647
758
Example steel




AC






0.0021


643
718
Example steel




AD







0.028

671
775
Example steel




AE








0.0025
637
752
Example steel





Underlined parts each indicate being out of the range of the present invention. — each indicate a content at an inevitable impurity level.



















TABLE 2









Finishing

Hot rolled
Re-
Cold rolled sheet




delivery
Average
sheet heat treatment
duction
annealing treatment

















temperature
coiling
Heat
Heat
ratio
Heat
Heat




in hot
temperature
treatment
treatment
in cold
treatment
treatment



Steel
rolling
in coil
temperature
time
rolling
temperature
time


No.
type
(° C.)
(° C.)
(° C.)
(s)
(%)
(° C.)
(s)





1
A
880
450
750
23400
55.6




2
A
900
475
770
28800
68.4




3
A
850
450
700
32400
58.8




4
A
880
500
650
36000
64.7




5
A
900
550
700
64800
61.1




6
A
860
520
720
23400
60.0




7
A
870
480
700
32400
56.3




8
A
890
510
720
39600
58.8




9
A
880
500
680
23400
57.6
750
490


10
B
900
520
690
28800
48.4
720
300


11
C
850
540
720
32400
47.1
690
270


12
A

700

500
720
43200
70.6
740
180


13
A
870

860

700
32400
47.8
680
600


14
A
880
580

480

36000
58.8
700
700


15
A
890
490

840

36000
64.7
680
500


16
A
890
600
700
7200
53.8
750
350


17
A
880
590
660
23400
64.7

520

550


18
A
880
560
680
108000 
50.0
700
15


19
A
860
560
700
57600
51.7
740

920



20
A
870
550
680
64800
64.7
720
300


21
A
850
480
720
36000
63.2
750
350


22
A
840
400
640
32400
66.7
680
250


23
A
910
600
700
23400
58.8
720
330


24
A
880
480
720
28800
64.7
700
300


25
A
890
560
700
32400
64.7
720
240


26
A
910
500
680
43200
66.7
680
360


27
A
900
520
700
32400
66.7
750
280


28
D
870
620
680
43200
58.8
750
360


29
E
900
590
710
28800
58.8
650
450


30
F
900
590
730
57600
58.8
680
600


31
F
910
550
720
23400
58.8
700
540


32
G
880
600
700
32400
52.9
820
480


33
H
870
560
680
32400
47.1
780
450


34
I
900
580
690
36000
60.0
770
240


35
J
890
600
670
23400
53.8
750
260


36
K
870
610
700
28800
62.5
720
300


37
K
880
 53
720
23400
56.3
740
360


38
L
850
560
680
32400
58.8
650
240


39
M
900
580
690
23400
62.5
730
360


40
N
860
510
700
36000
62.5
700
300


41
O
850
600
680
28800
58.8
750
390


42
P
840
550
660
57600
50.0
750
270


43
Q
860
550
690
32400
38.5
700
300


44
R
850
560
700
39600
47.1
740
250


45
S
870
610
720
23400
52.9
720
300


46
T
840
540
730
28800
61.1
770
340


47
U
870
520
700
57600
56.3
750
600


48
V
880
500
720
23400
64.7
740
500


49
W
900
500
690
28800
64.7
740
500


50
X
900
600
700
57600
56.3
680
250


51
Y
920
580
720
23400
62.5
710
300


52
Z
900
560
700
23400
45.2
730
340


53
AA
860
550
680
108000 
56.3
680
500


54
AB
850
540
710
28800
56.3
750
250


55
AC
880
520
690
36000
62.5
770
300


56
AD
840
520
750
32400
64.7
720
340


57
AE
820
500
680
39600
55.6
780
360


















Cold rolled sheet
Cold rolled sheet







annealing treatment
annealing treatment




















Heat
Heat
Heat
Heat
Galvan-






treatment
treatment
treatment
treatment
nealing






temperature
time
temperature
time
temperature





No.
(° C.)
(s)
(° C.)
(s)
(° C.)
Type *
Remarks






1
710
280
200
 7200

CR
Example



2
730
300
100
21600
520
GA
Example



3
740
270
260
 9000

GI
Example



4
790
270
 80
21600

CR
Example



5
800
320
200
14400
520
GA
Example



6
810
300
240
10800

GI
Example



7

560

250
240
14400

GI
Comparative










example



8

920

420
220
 5400
530
GA
Comparative










example



9
700
480
300
 3600

GI
Example



10
680
300
250
 7200
540
GA
Example



11
720
330
110
30000

CR
Example



12
700
240
 90
42000

GI
Comparative










example



13
710
500
100
32400
510
GA
Comparative










example



14
680
480
270
 6000

CR
Comparative










example



15
740
240
210
 9000

GI
Comparative










example



16
750
600
 70
32400
460
GA
Comparative










example



17
680
550
190
 7200
550
GA
Comparative










example



18
700
600
140
 9600

CR
Comparative










example



19
710
360
290
 3600
530
GA
Comparative










example



20

550

300
170
10800

GI
Comparative










example



21

880

280
190
14400
500
GA
Comparative










example



22
700
10
230
24000
520
GA
Comparative










example



23
740

1800

 70
18000

CR
Comparative










example



24
660
190
 30
32400
520
GA
Comparative










example



25
700
300
450
15000
550
GA
Comparative










example



26
665
180
140
600
500
GA
Comparative










example



27
710
280
130

86400

470
GA
Comparative










example



28
780
300
200
39600

CR
Example



29
680
270
130
 5400
550
GA
Example



30
740
300
280
 1800

CR
Example



31
730
330
170
 7200
580
GA
Example



32
700
400
290
 9600

GI
Example



33
660
450
120
19200

CR
Example



34
750
650
 80
10800

GI
Example



35
690
200
290
18000

GI
Comparative










example



36
760
250
120
 7200

CR
Comparative










example



37
770
250
110
14400
570
GA
Comparative










example



38
630
300
280
 7200
580
GA
Comparative










example



39
700
240
250
42000
540
GA
Example



40
680
420
280
30000

CR
Comparative










example



41
700
300
190
32400

GI
Example



42
720
240
170
 6000

CR
Example



43
730
480
280
 9000
520
GA
Example



44
740
420
200
32400

CR
Example



45
700
300
 75
 7200
520
GA
Example



46
680
300
 90
 9600
500
GA
Example



47
750
200
210
 3600

GI
Example



48
690
250
100
10800

GI
Example



49
710
270
 60
14400

GI
Example



50
700
250
120
24000
520
GA
Example



51
750
300
220
18000

GI
Example



52
710
340
 90
14400
480
GA
Example



53
690
600
300
24000

GI
Example



54
680
450
280
18000
520
GA
Example



55
750
420
120
12000

CR
Example



56
700
360
230
 7200

GI
Example



57
6701
300
 80
42000

CR
Example





Underlined parts each indicate being out of the range of the present invention.


* CR: Cold rolled steel sheet (without coating), GI: Hot-dip galvanized steel sheet (galvanization without galvannealing treatment), GA: Hot-dip galvannealed steel sheet


1) Holding for 20 s or more and 900 s or less within a temperature range of an Ac1 transformation temperature or more


2) Holding for 20 s or more and 900 s or less within a temperature range of an Ac1 transformation temperature or more and the Ac1 transformation temperature + 150° C. or less



























TABLE 3

















Average


Average













Mn


C











Average
Average
content
Average
Average
content
Area








Average
Average
Mn
Mn
in RA/
C
C
in RA/
fraction




Sheet
Area
Area
Volumne
grain
grain
content
content
average
content
content
average
of




thick-
fraction
fraction
fraction
size of
size of
in RA
in F
MN
in RA
in F
C
blocky



Steel
ness
of F
of TM
of RA
F
RA
(% by
(% by
content
(% by
(% by
content
RA


No.
type
(mm)
(%)
(%)
(%)
(μm)
(μm)
mass)
mass)
in F
mass)
mass)
in F
(%)





1
A
1.6
55.6
16.1
20.6
5.7
1.1
5.90
1.25
4.72
0.47
0.06
7.72
18.3


2
A
1.2
54.5
15.2
21.4
4.9
2.2
6.14
5.08
2.95
0.38
0.04
9.50
16.2


3
A
1.4
58.3
14.8
21.4
4.1
1.8
5.68
1.93
2.94
0.36
0.06
8.22
17.8


4
A
1.2
61.2
19.8
15.6
2.2
1.3
4.94
2.89
1.71
0.29
0.08
3.63
14.0


5
A
1.4
59.4
18.6
13.9
5.3
2.7
4.69
2.69
1.74
0.30
0.09
3.33
13.3


6
A
1.2
59.2
19.2
13.1
5.1
1.7
4.61
2.67
1.73
0.27
0.06
4.50
12.1


7
A
1.4

85.0

4.3
6.4
4.8
2.3
3.82
3.05

1.25

0.14
0.09

1.56

 5.0


8
A
1.4
43.9

46.8

3.8
3.2
0.9
3.85
3.19

1.21

0.16
0.11

1.45

 3.1


9
A
1.4
56.5
18.9
20.6
3.5
0.8
6.98
2.57
2.72
0.35
0.07
5.13
16.2


10
B
1.6
65.3
13.5
16.8
2.0
2.4
6.12
2.98
2.05
0.39
0.05
7.45
16.6


11
C
1.8
59.7
17.7
21.0
2.8
1.3
6.73
2.13
3.15
0.45
0.05
8.48
17.9


12
A
1.0
54.0
16.7
19.9
8.8
2.8
5.58
1.32
4.21
0.18
0.05
3.88
15.3


13
A
1.2
61.2
15.5
13.4

7.6


4.8

6.04
1.46
4.14
0.29
0.07
4.14
10.9


14
A
1.4
50.8

32.7

6.5
2.5
1.1
4.09
3.16

1.29

0.28
0.10
2.80
 5.8


15
A
1.2
61.0

26.9

6.1
2.5
0.4
4.28
3.31

1.29

0.40
0.08
5.15
 5.6


16
A
1.2
61.5

30.2

5.8
4.0
0.5
3.94
3.10

1.27

0.30
0.07
4.21
 4.9


17
A
1.2
69.4
18.0
6.6
2.9
2.7
4.29
3.35

1.28

0.29
0.03
9.38
 4.5


18
A
1.4
63.7
15.8
5.8
2.7
1.2
4.44
3.22

1.36

0.29
0.04
7.19
 5.5


19
A
1.4
61.8

29.4

7.2
4.4
1.7
3.99
3.15

1.27

0.21
0.05
4.11
 6.0


20
A
1.2

83.1

10.8
4.2
4.8
1.5
5.22
2.47
2.11
0.41
0.09
4.56
 3.5


21
A
1.4
53.8

35.8

6.9
4.2
2.8
4.05
3.19

1.27

0.48
0.07
6.89
 6.0


22
A
1.2

84.5

 8.6
5.4
2.9
0.8
7.16
1.47
4.87
0.35
0.05
7.39
 4.2


23
A
1.4
83.1
37.5
6.3
4.7
1.2
4.03
3.25

1.24

0.52
0.08
6.13
 5.3


24
A
1.2

82.7

1.1
11.3
4.5
1.1
6.89
2.04
3.38
0.41
0.08
5.13
10.4


25
A
1.2
55.3
12.8
5.4
4.6
1.3
6.99
2.03
3.44
0.39
0.04
9.75
 4.4


26
A
1.2

81.4

1.3
12.5
4.4
1.2
6.48
2.08
3.12
0.40
0.05
8.00
10.5


27
A
1.2
54.3
14.5
6.1
4.7
1.2
6.85
2.10
3.26
0.42
0.07
8.00
 4.3


28
D
1.4
57.7
19.6
19.8
5.2
1.4
6.17
3.15
1.96
0.54
0.07
7.71
17.3


29
E
1.4
54.0
19.3
20.9
5.9
1.1
6.85
3.55
1.93
0.30
0.06
5.00
17.2


30
F
1.4
52.6
17.2
20.3
3.8
2.8
7.47
1.38
5.41
0.61
0.06
9.98
17.9


31
F
1.4
52.4
18.1
19.6
3.7
2.6
7.44
1.36
5.47
0.59
0.07
8.43
17.4


32
G
1.4
50.2
19.5
23.0
4.5
1.5
4.03
2.20
1.83
0.28
0.04
6.75
16.4


33
H
1.6
54.5
14.3
21.5
3.6
1.4
7.27
2.02
3.60
0.31
0.06
5.35
18.6


34
I
1.8
56.8
15.8
18.2
5.4
2.4
5.41
2.85
1.90
0.43
0.05
8.65
14.4


35
J
1.4

83.4

 5.1
3.1
2.6
0.9
6.67
2.73
2.44
0.19
0.02
9.28
 2.8


36
K
1.2
56.9
17.9
19.2
2.8
0.4
7.40
2.90
2.55
0.28
0.07
3.89
16.2


37
K
1.2
57.2
18.3
19.0
2.9
0.5
7.43
2.55
2.91
0.31
0.06
5.17
17.3


38
L
1.2
56.9
17.9
15.4
2.4
1.2
6.54
2.66
2.46
0.39
0.04
9.19
10.9


39
M
1.4
54.4
19.3
18.8
3.1
1.8
7.17
1.91
3.75
0.32
0.04
7.97
12.6


40
N
1.4
60.0
18.8
18.4
4.1
1.2
7.13
2.51
2.84
0.36
0.06
5.80
12.2


41
O
1.2
53.3
15.8
21.2
4.0
0.7
6.50
1.67
3.89
0.30
0.06
4.99
13.6


42
P
1.2
52.9
16.6
20.6
4.5
0.6
6.14
2.41
2.55
0.43
0.05
8.55
15.8


43
Q
1.4
53.1
18.9
20.8
2.9
0.7
7.00
2.27
3.08
0.31
0.05
6.20
15.0


44
R
1.4
55.0
19.3
20.5
2.4
0.3
7.58
1.25
6.06
0.45
0.06
7.58
15.8


45
S
1.6
54.5
19.9
21.0
3.1
1.0
7.33
1.66
4.42
0.49
0.06
7.84
16.2


46
T
1.8
58.3
16.4
18.2
5.2
2.6
6.70
2.17
3.09
0.42
0.05
8.40
15.3


47
U
1.6
63.9
10.5
21.6
4.3
2.0
5.43
3.33
1.63
0.34
0.04
8.18
14.1


48
V
1.4
53.4
17.8
19.2
4.3
0.6
6.74
2.74
2.46
0.43
0.05
8.60
17.9


49
W
1.4
56.6
17.4
19.0
3.6
0.8
5.97
2.52
2.37
0.47
0.06
7.85
17.7


50
X
1.2
51.2
19.2
19.8
4.5
2.4
6.41
2.73
2.35
0.45
0.05
9.00
14.1


51
Y
1.2
55.5
18.9
19.6
5.6
2.8
7.10
2.79
2.54
0.54
0.09
6.20
17.5


52
Z
1.4
52.8
19.0
19.8
2.3
1.3
5.95
3.46
1.72
0.45
0.06
7.50
17.0


53
AA
1.2
53.2
18.6
18.4
5.0
2.7
6.92
2.62
2.54
0.42
0.05
8.40
13.8


54
AB
1.4
59.9
18.8
19.7
3.7
2.6
6.04
3.01
2.01
0.50
0.06
7.79
15.1


55
AC
1.4
54.7
19.7
21.5
2.6
0.8
6.84
2.84
2.38
0.47
0.07
6.71
14.9


56
AD
1.4
54.6
19.0
21.4
4.7
2.4
5.49
2.84
1.93
0.53
0.07
7.57
13.2


57
AE
1.2
57.3
19.7
21.0
4.5
1.8
6.92
3.75
1.85
0.23
0.07
3.27
15.0









Area
















fraction of
















blocky
















RA/(area
















fraction















Area
of blocky
Intra-














fraction
RA +
steel






Chemical







of
area
hydrogen




λ
λ
conver-







lath-like
fraction
amount



TS × EL
(Punch-
(Ream-
sion







RA
of lath-like
(ppm
Other
TS
EL
(MPA ·
ing)
er)
treata-
Coata-





No.
(%)
RA)
by mass)
phases
(MPa)
(%)
%)
(%)
(%)
bility
bility
Remarks







1
2.3
0.89
0.14
BF,
 992
23.9
23709
26
52
5

Example








MP, θ












2
5.2
0.76
0.20
BF,
1012
21.6
21859
23
55

Good
Example








MP, θ












3
3.6
0.83
0.17
BF,
1005
23.0
23115
24
56

Good
Example








MP, θ












4
1.6
0.90
0.24
BF,
1191
13.9
16555
17
57
5

Example








MP, θ












5
0.5
0.96
0.10
BF,
1225
12.5
15313
16
59

Good
Example








MP, θ












6
1.0
0.92
0.24
BF,
1240
12.3
15252
15
55

Good
Example








MP, θ












7
3.4
0.60
0.17
BF,
810

15.7

25106
27
53

Good
Comparative








MP, θ







example




8
0.7
0.82
0.20
BF,
1440
 8.1
11664
13
44

Good
Comparative








MP, θ







example




9
4.4
0.79
0.21
BF,
 996
21.9
21812
25
51

Good
Example








MP, θ












10
0.2
0.99
0.27
BF,
 989
23.5
23242
26
49

Good
Example








MP, θ












11
3.1
0.85
0.13
BF,
1193
12.9
15390
18
53
4

Example








MP, θ












12
4.6
0.77
0.13
BF,
865

11.9

18541
24
49

Good
Comparative








MP, θ







example




13
2.5
0.81
0.21
BF,
844

15.5

13082
16
52

Good
Comparative








MP, θ







example




14
0.7
0.89
0.16
BF,
1051

12.1

12717
20
59
5

Comparative








MP, θ







example




15
0.5
0.92
0.14
BF,
1214

10.7

12990
16
56

Good
Comparative








MP, θ







example




16
0.9
0.84
0.14
BF,
1243

10.1

12554
15
61

Good
Comparative








MP, θ







example




17
2.1
0.68
0.23
BF,
1002

17.1

17134
22
57

Good
Comparative








MP, θ







example




18
0.3
0.95
0.11
BF,
 988

16.3

16104
22
59
5

Comparative








MP, θ







example




19
1.2
0.83
0.17
BF,
1106

11.4

12608
20
47

Good
Comparative








MP, θ







example




20
0.7
0.83
0.21
BF,
820

19.2

23944
30
60

Good
Comparative








MP, θ







example




21
0.9
0.87
0.16
BF,
1257

10.7

13450
11
47

Good
Comparative








MP, θ







example




22
1.2
0.78
0.09
BF,
 847

17.5

24987
27
54
5
Good
Comparative








MP, θ







example




23
1.0
0.84
0.12
BF,
1297

11.7

11922

10

54


Comparative








MP, θ







example




24
0.9
0.92

0.45

BF,
803
23.5
18871

14

39

Good
Comparative








MP, θ







example




25
1.0
0.81
0.06
BF,
 968

11.4

11229
21
60

Good
Comparative








MP, θ







example




26
2.0
0.84

0.52

BF,
815
24.2
19723

14

39

Good
Comparative








MP, θ







example




27
1.8
0.70
0.04
BF,
 991

13.2

13081
20
60

Good
Comparative








MP, θ







example




28
2.5
0.87
0.23
BF,
1208
17.5
21140
10
54
4

Example








MP, θ












29
3.7
0.82
0.23
BF,
1003
20.7
20782
26
43

Good
Example








MP, θ












30
2.4
0.88
0.24
BF,
1120
20.0
22400
20
49
4

Example








MP, θ












31
2.2
0.89
0.20
BF,
1121
19.2
21523
21
52

Fair
Example








MP, θ












32
6.6
0.71
0.24
BF,
 986
22.4
22086
23
61

Good
Example








MP, θ












33
2.9
0.87
0.23
BF,
1070
25.6
27392
24
60
4

Example








MP, θ












34
3.8
0.79
0.09
BF,
 981
20.8
20405
25
49

Good
Example








MP, θ












35
0.3
0.90
0.17
BF,
548
31.4
17207
62
58

Good
Comparative








MP, θ







example




36
3.0
0.84
0.18
BF,
1001

13.4

13413

12

51
2

Comparative








MP, θ







example




37
1.7
0.91
0.13
BF,
 997

13.1

13061

13

52

Poor
Comparative








MP, θ







example




38
4.5
0.71
0.10
BF,
1022
25.3
25857
22
62

Poor
Comparative








MP, θ







example




39
6.2
0.67
0.12
BF,
1001
23.5
23524
24
56

Good
Example








MP, θ












40
6.2
0.66
0.29
BF,
 994
21.3
21172

13

52
5

Comparative








MP, θ







example




41
7.6
0.64
0.12
BF,
 988
22.8
22526
23
52

Good
Example








MP, θ












42
4.8
0.77
0.16
BF,
1083
19.2
20794
20
56
4

Example








MP, θ












43
5.8
0.72
0.21
BF,
1102
18.7
20607
20
53

Good
Example








MP, θ












44
4.7
0.77
0.22
BF,
1123
17.5
19653
22
58
5

Example








MP, θ












45
4.8
0.77
0.10
BF,
1000
23.9
23900
25
56

Good
Example








MP, θ












46
2.9
0.84
0.24
BF,
 983
22.2
21823
23
55

Good
Example








MP, θ












47
7.5
0.65
0.19
BF,
1093
17.7
19346
20
51

Good
Example








MP, θ












48
1.3
0.93
0.23
BF,
 992
23.6
23411
23
59

Good
Example








MP, θ












49
1.3
0.93
0.28
BF,
 995
23.7
23582
22
59

Good
Example








MP, θ












50
5.7
0.71
0.19
BF,
1033
23.1
23862
27
60

Good
Example








MP, θ












51
2.1
0.89
0.09
BF,
1100
18.4
20240
19
62

Good
Example








MP, θ












52
2.8
0.86
0.22
BF,
1113
13.9
15460
18
63

Good
Example








MP, θ












53
4.6
0.75
0.15
BF,
1051
21.4
22491
24
61

Good
Example








MP, θ












54
4.6
0.77
0.22
BF,
1080
19.9
21492
20
62

Good
Example








MP, θ












55
6.6
0.89
0.16
BF,
1199
15.1
18105
15
63
4

Example








MP, θ












56
8.2
0.82
0.09
BF,
1011
21.5
21737
24
59

Good
Example








MP, θ












57
6.0
0.71
0.28
BF,
 995
21.0
20895
25
51
4

Example








MP, θ









The Ac1 transformation temperature and the Ac3 transformation temperature were determined using the following expressions.

The Ac1 transformation temperature (° C.)=751−16×(% C)+11×(% Si)−28×(% Mn)−5.5×(% Cu)−16×(% Ni)+13×(% Cr)+3.4×(% Mo)
The Ac3 transformation temperature (° C.)=910−203√(% C)+45×(% Si)−30×(% Mn)−20×(% Cu)−15×(% Ni)+11×(% Cr)+32×(% Mo)+104×(% V)+400×(% Ti)+200×(% Al)


Where (% C), (% Si), (% Mn), (% Ni), (% Cu), (% Cr), (% Mo), (% V), (% Ti), and (% Al) are respective contents (% by mass) of the elements.


A tensile test was conducted pursuant to JIS Z 2241 (2011) using a JIS No. 5 test piece sampled so as to cause a tensile direction to be a right-angle direction relative to a rolling direction of the steel sheets to measure tensile strength (TS) and total elongation (EL). The mechanical properties were determined to be favorable in the following cases.


TS of 980 MPa or more and less than 1,080 MPa, EL≥20%


TS of 1,080 MPa or more and less than 1,180 MPa, EL≥16%


TS of 1,180 MPa or more and less than 1,270 MPa, EL≥12%


The hole expandability was evaluated pursuant to JIS Z 2256 (2010). Each of the obtained steel sheets was cut into 100 mm×100 mm, then a hole with a diameter of 10 mm was punched with a clearance of 12%±1%, or a hole was shaved to be enlarged to a hole with a diameter of 10 mm by reaming, then while being pressed with a blank holder force of 9 tons using a die with an inner diameter of 75 mm, a 60° conical punch was pressed into the hole to measure a hole diameter at a crack occurrence limit, a limit hole expansion ratio λ (%) was determined from the following expression, and the hole expandability was evaluated from the value of this limit hole expansion ratio λ. The reaming refers to shaving and enlarging an inner diameter machined with a drill to a certain hole dimension with a cutting blade part and, in addition, finishing a machined face while grinding it down with a margin part.

Limit hole expansion ratio λ(%)={(Df−D0)/D0}×100


Where Df is a hole diameter (mm) at the time of occurrence of a crack, whereas Do is an initial hole diameter (mm). In the present invention, the following cases were determined to be favorable for each TS range.


TS of 980 MPa or more and less than 1,080 MPa, (punching) λ≥15%, (reaming) λ≥40%


TS of 1,080 MPa or more and less than 1,180 MPa, (punching) λ≥12%, (reaming) λ≥35%


TS of 1,180 MPa or more and less than 1,270 MPa, (punching) λ≥10%, (reaming) λ≥30%


The chemical conversion treatability was evaluated by forming a chemical conversion film by performing chemical conversion treatment by the following method using a chemical conversion treatment liquid (Palbond L3080 (registered trademark)) manufactured by Nihon Parkerizing Co., Ltd. on the obtained cold rolled steel sheet. Specifically, first, the obtained cold rolled steel sheet was degreased using a degreasing liquid Fine Cleaner (registered trademark) manufactured by Nihon Parkerizing Co., Ltd. and was then washed with water. Next, using a surface conditioner Prepalene Z (registered trademark) manufactured by Nihon Parkerizing Co., Ltd., surface conditioning with 30 seconds was performed. The cold rolled steel sheet subjected to the surface conditioning was immersed in a 43° C. chemical conversion treatment liquid (Palbond L3080) for 120 seconds, was then washed with water, and was dried with hot air. Thus, the cold rolled steel sheet was subjected to the chemical conversion treatment. For a surface of the cold rolled steel sheet after the chemical conversion treatment, five fields of view were randomly observed with a 500-fold magnification using a SEM. An area fraction [%] of areas with no chemical conversion film formed (voids) was determined by image processing, and the following evaluation was performed depending on the determined area fraction. With Mark 4 or Mark 5, the chemical conversion treatability can be said to be favorable. Among them, Mark 5 is preferred.


Mark 5: 5% or less


Mark 4: greater than 5% and 10% or less


Mark 3: greater than 10% and 25% or less


Mark 2: greater than 25% and 40% or less


Mark 1: greater than 40%


The coatability was determined through appearance. A case in which appropriate surface quality was ensured without faulty appearance including uncoating, alloying unevenness, and other defects impairing surface quality was determined to be “good”, a case in which minor defects were partially found was determined to be “fair”, and a case in which many surface defects were found was determined to be “poor”.


As is clear from Table 3, in all the examples, high-strength steel sheets having a TS of 980 MPa or more and being excellent in formability were obtained. On the other hand, in the comparative examples, they were inferior in at least one characteristic of TS, EL, λ, the chemical conversion treatability, and the coatability.


INDUSTRIAL APPLICABILITY

The present invention can provide a high-strength steel sheet having a tensile strength (TS) of 980 MPa or more and having excellent formability and a method for manufacturing the same.

Claims
  • 1. A high-strength steel sheet comprising: a component composition including: by mass %, C: 0.030% to 0.250%; Si: 0.01% to 3.00%; Mn: 3.10% to 4.20%; P: 0.001% to 0.100%; S: 0.0001% to 0.0200%; N: 0.0005% to 0.0100%; Al: 0.010% to 1.200%; and balance Fe and inevitable impurities; anda steel structure with: ferrite being 35% to 80% and tempered martensite being greater than 5% and 20% or less in terms of area fraction;retained austenite being 8% or more in terms of volume fraction;an average grain size of the ferrite being 6 μm or less;an average grain size of the retained austenite being 3 μm or less;a value obtained by dividing an area fraction of blocky austenite by a sum of area fractions of lath-like austenite and the blocky austenite being 0.6 or more;a value obtained by dividing an average Mn content, by mass %, in the retained austenite by an average Mn content, by mass %, in the ferrite being 1.5 or more; anda value obtained by dividing an average C content, by mass %, in the retained austenite by an average C content, by mass %, in the ferrite being 3.0 or more,wherein the high-strength steel sheet has a tensile strength of 980 MPa or more.
  • 2. The high-strength steel sheet according to claim 1, wherein the high-strength steel sheet includes a diffusible hydrogen amount in steel of 0.3 ppm by mass or less, the diffusible hydrogen being hydrogen having a temperature of 300° C. or less in a test piece of the steel sheet subject to annealing with a length of 30 mm and a width of 5 mm, and from which a plated layer was polished to be removed.
  • 3. The high-strength steel sheet according to claim 2, wherein the component composition further includes: by mass %, at least one element selected from Ti: 0.005% to 0.200%; Nb: 0.005% to 0.200%; V: 0.005% to 0.500%; W:0.005% to 0.500%; B: 0.0003% to 0.0050%; Ni: 0.005% to 1.000%; Cr: 0.005% to 1.000%; Mo: 0.005% to 1.000%; Cu: 0.005% to 1.000%; Sn: 0.002% to 0.200%; Sb: 0.002% to 0.200%; Ta: 0.001% to 0.100%; Ca: 0.0005% to 0.0050%; Mg: 0.0005% to 0.0050%; Zr: 0.0005% to 0.0050%; and REM: 0.0005% to 0.0050%.
  • 4. The high-strength steel sheet according to claim 3, wherein the component composition further includes: by mass %, at least one element selected from Ti: 0.005% to 0.200%; Nb: 0.005% to 0.200%; V: 0.005% to 0.500%; W:0.005% to 0.500%; B: 0.0003% to 0.0050%; Ni: 0.005% to 1.000%; Cr: 0.005% to 1.000%; Mo: 0.005% to 1.000%; Cu: 0.005% to 1.000%; Sn: 0.002% to 0.200%; Sb: 0.002% to 0.200%; Ta: 0.001% to 0.100%; Ca: 0.0005% to 0.0050%; Mg: 0.0005% to 0.0050%; Zr: 0.0005% to 0.0050%; and REM: 0.0005% to 0.0050%.
Priority Claims (1)
Number Date Country Kind
2018-066730 Mar 2018 JP national
PCT Information
Filing Document Filing Date Country Kind
PCT/JP2019/011648 3/20/2019 WO
Publishing Document Publishing Date Country Kind
WO2019/188642 10/3/2019 WO A
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Related Publications (1)
Number Date Country
20210010101 A1 Jan 2021 US