HIGH-STRENGTH STEEL SHEET AND METHOD FOR MANUFACTURING SAME

Information

  • Patent Application
  • 20170204491
  • Publication Number
    20170204491
  • Date Filed
    August 05, 2015
    10 years ago
  • Date Published
    July 20, 2017
    8 years ago
Abstract
Disclosed is a method comprising: preparing a steel slab with a predetermined chemical composition; subjecting the steel slab to hot rolling by heating it to a temperature of 1100-1300° C., hot rolling it with a finisher delivery temperature of 800-1000° C. to form a hot-rolled steel sheet, and coiling the steel sheet at a mean coiling temperature of 200-500° C.; subjecting the steel sheet to pickling treatment; subjecting the steel sheet to annealing by retaining the steel sheet at a temperature of 740-840° C. for 10-900 s, and the cooling the steel sheet at a mean cooling rate of 5-30° C./s to a cooling stop temperature of 150-350° C.; and subjecting the steel sheet to reheating treatment by reheating the steel sheet to a reheating temperature of higher than 350° C. and 550° C. or lower, and retaining the steel sheet at the reheating temperature for 10 s or more.
Description
TECHNICAL FIELD

This disclosure relates to a high-strength steel sheet with excellent formability which is mainly suitable for automobile structural members and a method for manufacturing the same, and in particular, to provision of a high-strength steel sheet with high productivity that has a tensile strength (TS) of 780 MPa or more and that is excellent in ductility as well as in stretch flangeability and fatigue properties.


BACKGROUND

In order to secure passenger safety upon collision and to improve fuel efficiency by reducing the weight of automotive bodies, high-strength steel sheets reduced in thickness and having a tensile strength (TS) of 780 MPa or more have been increasingly applied to automobile structural members. Further, in recent years, examination has been made of applications of ultra-high-strength steel sheets with 980 MPa and 1180 MPa grade TS.


In general, however, strengthening of steel sheets leads to deterioration in formability. It is thus difficult to achieve both increased strength and excellent formability. Therefore, it is desirable to develop steel sheets with increased strength and excellent formability.


It is also desirable for steel sheets to have excellent fatigue properties since the travelable distance (total running distance) of automobiles depends on the fatigue strength of steel sheets applied to the automobile structural members.


To meet these demands, for example, JP2004218025A (PTL 1) describes “a high-strength steel sheet with excellent workability and shape fixability comprising: a chemical composition containing, in mass %, C: 0.06% to 0.6%, Si+Al: 0.5% to 3%, Mn: 0.5% to 3%, P: 0.15% or less (exclusive of 0%), and S: 0.02% or less (inclusive of 0%); and a structure that contains tempered martensite: 15% or more by area to the entire structure, ferrite: 5% to 60% by area to the entire structure, and retained austenite: 5% or more by volume to the entire structure, and that may contain bainite and/or martensite, wherein a ratio of the retained austenite transforming to martensite upon application of a 2% strain is 20% to 50%.


JP2011195956A (PTL 2) describes “a high-strength thin steel sheet with excellent elongation and hole expansion formability, comprising: a chemical composition containing, in mass %, C: 0.05% or more and 0.35% or less, Si: 0.05% or more and 2.0% or less, Mn: 0.8% or more and 3.0% or less, P: 0.0010% or more and 0.1% or less, S: 0.0005% or more and 0.05% or less, N: 0.0010% or more and 0.010% or less, and Al: 0.01% or more and 2.0% or less, and the balance consisting of iron and incidental impurities; and a metallographic structure that includes a dominant phase of ferrite, bainite, or tempered martensite, and a retained austenite phase in an amount of 3% or more and 30% or less, wherein at a phase interface at which the austenite phase comes in contact with the ferrite phase, bainite phase, and martensite phase, a mean carbon concentration in the austenite phase is 0.6% or more and 1.2% or less, and austenite grains that satisfy Cgb/Cgc>1.3 are present in the austenite phase in an amount of 50% or more, where Cgc is a central carbon concentration and Cgb is a carbon concentration at grain boundaries of austenite grains.


JP201090475A (PTL 3) describes “a high-strength steel sheet comprising a chemical composition containing, in mass %, C: 0.17% or more and 0.73% or less, Si: 3.0% or less, Mn: 0.5% or more and 3.0% or less, P: 0.1% or less, S: 0.07% or less, Al: 3.0% or less, and N: 0.010% or less, where Si+Al is 0.7% or more, and the balance consisting of Fe and incidental impurities; and a structure that contains martensite: 10% or more and 90% or less by area to the entire steel sheet structure, retained austenite content: 5% or more and 50% or less, and bainitic ferrite in upper bainite: 5% or more by area to the entire steel sheet structure, wherein the steel sheet satisfies conditions that 25% or more of the martensite is tempered martensite, a total of the area ratio of the martensite to the entire steel sheet structure, the retained austenite content, and the area ratio of the bainitic ferrite in upper bainite to the entire steel sheet structure is 65% or more, and an area ratio of polygonal ferrite to the entire steel sheet structure is 10% or less (inclusive of 0%), and wherein the steel sheet has a mean carbon concentration of 0.70% or more in the retained austenite and has a tensile strength of 980 MPa or more.


JP2008174802A (PTL 4) describes “a high-strength cold-rolled steel sheet with a high yield ratio and having a tensile strength of 980 MPa or more, the steel sheet comprising, on average, a chemical composition that contains, by mass %, C: more than 0.06% and 0.24% or less, Si≦0.3%, Mn: 0.5% to 2.0%, P≦0.06%, S≦0.005%, Al≦0.06%, N≦0.006%, Mo: 0.05% to 0.5%, Ti: 0.03% to 0.2%, and V: more than 0.15% and 1.2% or less, and the balance consisting of Fe and incidental impurities, wherein the contents of C, Ti, Mo, and V satisfy 0.8≦(C/12)/{(Ti/48)+(Mo/96)+(V/51)}≦1.5, and wherein an area ratio of ferrite phase is 95% or more, and carbides containing Ti, Mo, and V with a mean grain size of less than 10 nm are diffused and precipitated, where Ti, Mo, and V contents represented by atomic percentage satisfy V/(Ti+Mo+V)≧0.3.


JP2010275627A (PTL 5) describes “a high-strength steel sheet with excellent workability comprising a chemical composition containing C: 0.05 mass % to 0.3 mass %, Si: 0.01 mass % to 2.5 mass %, Mn: 0.5 mass % to 3.5 mass %, P: 0.003 mass % to 0.100 mass %, S: 0.02 mass % or less, and Al: 0.010 mass % to 1.5 mass %, where a total of the Si and Al contents is 0.5 mass % to 3.0 mass %, and the balance consisting of Fe and incidental impurities; and a metallic structure that contains, by area, ferrite: 20% or more, tempered martensite: 10% to 60%, and martensite: 0% to 10%, and that contains, by volume, retained austenite: 3% to 10%, where a ratio (m)/(f) of a Vickers hardness (m) of the tempered martensite to a Vickers hardness (f) of the ferrite is 3.0 or less.


JP4268079B (PTL 6) describes “an ultra-high-strength steel sheet exhibiting an excellent elongation in an ultra-high-strength range with a tensile strength of 1180 MPa or more, and having excellent hydrogen embrittlement resistance, the steel sheet comprising a chemical composition containing, in mass %, C: 0.06% to 0.6%, Si+Al: 0.5% to 3%, Mn: 0.5% to 3%, P: 0.15% or less (exclusive of 0%), S: 0.02% or less (inclusive of 0%), and the balance: Fe and incidental impurities; and a structure that contains tempered martensite: 15% to 60% by area to the entire structure, ferrite: 5% to 50% by area to the entire structure, retained austenite: 5% or more by area to the entire structure, and massive martensite with an aspect ratio of 3 or less: 15% to 45%, where an area ratio of fine martensite having a mean grain size of 5 μm or less in the massive martensite is 30% or more.


PTL 6 also describes a method for manufacturing the ultra-high-strength steel sheet comprising: heating and retaining a steel satisfying the aforementioned composition at a temperature from A3 to 1100° C. for 10 s or more, and then cooling the steel at a mean cooling rate of 30° C./s or higher to a temperature at or below Ms, and repeating this cycle at least twice; and heating and retaining the steel at a temperature from (A3-25° C.) to A3 for 120 s to 600 s, and then cooling the steel at a mean cooling rate of 3° C./s or higher to a temperature at or above Ms and at or below Bs, at which the steel is retained for at least one second.


CITATION LIST
Patent Literature

PTL 1: JP2004218025A


PTL 2: JP2011195956A


PTL 3: JP201090475A


PTL 4: JP2008174802A


PTL 5: JP2010275627A


PTL 6: JP4268079B


SUMMARY
Technical Problem

In fact, PTL 1 teaches the high-strength steel sheet has excellent workability and shape fixability, PTL 2 teaches the high-strength thin steel sheet has excellent elongation and hole expansion formability, PTL 3 teaches the high-strength steel sheet has excellent workability, in particular, excellent ductility and stretch flangeability. None of them however takes into account fatigue properties.


The high-strength cold-rolled steel sheet with a high yield ratio described in PTL 4 uses expensive elements, Mo and V, which results in increased costs and a low elongation (EL), which is as low as approximately 19%.


The high-strength steel sheet described in PTL 5 exhibits, for example, TS of 980 MPa or more and TS×EL of approximately 24000 MPa·%, which remain, although may be relatively high when compared to general-use material, insufficient to meet the ongoing requirements for steel sheets.


The ultra-high tensile-strength steel sheet described in PTL 6 requires performing annealing treatment at least three times during its manufacture, resulting in low productivity in actual facilities.


It could thus be helpful to provide a method that can manufacture a high-strength steel sheet with high productivity that has a tensile strength (TS) of 780 MPa or more and that is excellent not only in ductility but also in stretch flangeability and fatigue properties, by performing a single annealing treatment at a ferrite-austenite dual phase region to form a fine structure that contains appropriate amounts of ferrite, bainitic ferrite, and retained austenite, and performing reheating following the annealing treatment so that an appropriate amount of tempered martensite is present in the structure.


It could also be helpful to provide a high-strength steel sheet manufactured by the method.


As used herein, the term “high-strength steel sheet” is intended to include high-strength galvanized steel sheets having a galvanized surface.


A steel sheet obtained according to the disclosure has the following target properties:


Tensile strength (TS)

    • 780 MPa or more


Ductility

    • TS 780 MPa grade: EL≧34%
    • TS 980 MPa grade: EL≧27%
    • TS 1180 MPa grade: EL≧23%


Balance between strength and ductility

    • TS×EL≧27000 MPa·%


Stretch flangeability

    • TS 780 MPa grade: λ≧40%
    • TS 980 MPa grade: λ≧30%
    • TS 1180 MPa grade: λ≧20%
    • The maximum hole expansion ratio λ (%)={(Df−D0)/D0}×100, where Df is the hole diameter (mm) upon cracking and D0 is the initial hole diameter (mm).


Fatigue property

    • fatigue limit strength ≧400 MPa, and fatigue ratio ≧0.40
    • As used herein, the term “fatigue ratio” means a ratio of fatigue limit strength to tensile strength.


Solution to Problem

Upon carefully examining how to manufacture a steel sheet having TS of 780 MPa or more and excellent in ductility, stretch flangeability, and fatigue properties with high productivity, we discovered the following.

    • (1) To obtain a steel sheet having a tensile strength (TS) of 780 MPa or more and excellent in ductility, stretch flangeability, and fatigue properties, it is important to prepare an appropriate chemical composition and to form a structure that contains appropriate amounts of ferrite, bainitic ferrite, and retained austenite, and in which fine retained austenite and fine bainitic ferrite are distributed.
    • (2) In addition, to form such a structure, it is important to provide the steel sheet with a structure prior to annealing treatment in which a single phase structure of martensite, a single phase structure of bainite, or a martensite-bainite mixed structure is dominantly present, while controlling annealing treatment conditions properly.
    •  In this respect, in order for the steel sheet to have such a pre-annealing structure without subjection to separate annealing treatment, it is important to perform appropriate slab reheating and optimize hot rolling conditions, in particular, to keep the mean coiling temperature (CT) following hot rolling low.
    • (3) Moreover, when cold rolling is performed after hot rolling, it is important to set a low rolling reduction such that the resulting structure of the hot-rolled steel sheet in which a single phase structure of martensite, a single phase structure of bainite, or a martensite-bainite mixed phase structure is dominantly present will remain intact as much as possible.
    • (4) Additionally, to improve stretch flangeability, it is important for the structure to contain an appropriate amount of tempered martensite and, to this end, it is of importance to keep the cooling stop temperature after annealing low and perform subsequent reheating treatment under proper conditions.


      The disclosure is based on the aforementioned discoveries and further studies.


Specifically, the primary features of this disclosure are as described below.


1. A method for manufacturing a high-strength steel sheet, the method comprising: preparing a steel slab containing (consisting of), in mass %, C: 0.10% or more and 0.35% or less, Si: 0.50% or more and 2.50% or less, Mn: 2.00% or more and less than 3.50%, P: 0.001% or more and 0.100% or less, S: 0.0001% or more and 0.0200% or less, and N: 0.0005% or more and 0.0100% or less, and the balance consisting of Fe and incidental impurities; subjecting the steel slab to hot rolling by heating the steel slab to a temperature of 1100° C. or higher and 1300° C. or lower, hot rolling the steel slab with a finisher delivery temperature of 800° C. or higher and 1000° C. or lower to form a hot-rolled steel sheet, and coiling the hot-rolled steel sheet at a mean coiling temperature of 200° C. or higher and 500° C. or lower; subjecting the hot-rolled steel sheet to pickling treatment; subjecting the hot-rolled steel sheet to annealing by retaining the hot-rolled steel sheet at a temperature of 740° C. or higher and 840° C. or lower for 10 s or more and 900 s or less, and then cooling the hot-rolled steel sheet at a mean cooling rate of 5° C./s or higher and 30° C./s or lower to a cooling stop temperature of 150° C. or higher and 350° C. or lower; and subjecting the hot-rolled steel sheet to reheating treatment by reheating the hot-rolled steel sheet to a reheating temperature of higher than 350° C. and 550° C. or lower, and retaining the hot-rolled steel sheet at the reheating temperature for 10 s or more.


2. The method for manufacturing a high-strength steel sheet according to 1., the method further comprising prior to the annealing, cold rolling the hot-rolled steel sheet at a rolling reduction of less than 30% to form a cold-rolled steel sheet, wherein in the annealing, the cold-rolled steel sheet is retained at a temperature of 740° C. or higher and 840° C. or lower for 10 s or more and 900 s or less, and cooled at a mean cooling rate of 5° C./s or higher and 30° C./s or lower to a cooling stop temperature of 150° C. or higher and 350° C. or lower, and in the reheating treatment, the cold-rolled steel sheet is reheated to a reheating temperature of higher than 350° C. and 550° C. or lower and retained at the reheating temperature for 10 s or more.


3. The method for manufacturing a high-strength steel sheet according to 1. or 2., the method further comprising after the reheating treatment, subjecting the hot-rolled steel sheet or the cold-rolled steel sheet to galvanizing treatment.


4. The method for manufacturing a high-strength steel sheet according to any of 1. to 3., wherein the steel slab further contains, in mass %, at least one element selected from the group consisting of Ti: 0.005% or more and 0.100% or less and B: 0.0001% or more and 0.0050% or less.


5. The method for manufacturing a high-strength steel sheet according to any of 1. to 4., wherein the steel slab further contains, in mass %, at least one element selected from the group consisting of Al: 0.01% or more and 1.00% or less, Nb: 0.005% or more and 0.100% or less, Cr: 0.05% or more and 1.00% or less, Cu: 0.05% or more and 1.00% or less, Sb: 0.002% or more and 0.200% or less, Sn: 0.002% or more and 0.200% or less, Ta: 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, and REM: 0.0005% or more and 0.0050% or less.


6. A high-strength steel sheet comprising: a steel chemical composition containing (consisting of), in mass %, C: 0.10% or more and 0.35% or less, Si: 0.50% or more and 2.50% or less, Mn: 2.00% or more and less than 3.50%, P: 0.001% or more and 0.100% or less, S: 0.0001% or more and 0.0200% or less, and N: 0.0005% or more and 0.0100% or less, and the balance consisting of Fe and incidental impurities; and a steel structure that contains a total of 30% or more and 75% or less by area of ferrite and bainitic ferrite, 5% or more and 15% or less by area of tempered martensite, and 8% or more by volume of retained austenite, wherein the retained austenite has a mean grain size of 2 μm or less and the bainitic ferrite has a mean free path of 3 μm or less.


7. The high-strength steel sheet according to 6., wherein the steel chemical composition further contains, in mass %, at least one element selected from the group consisting of Ti: 0.005% or more and 0.100% or less and B: 0.0001% or more and 0.0050% or less.


8. The high-strength steel sheet according to 6. or 7., wherein the steel chemical composition further contains, in mass %, at least one element selected from the group consisting of Al: 0.01% or more and 1.00% or less, Nb: 0.005% or more and 0.100% or less, Cr: 0.05% or more and 1.00% or less, Cu: 0.05% or more and 1.00% or less, Sb: 0.002% or more and 0.200% or less, Sn: 0.002% or more and 0.200% or less, Ta: 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, and REM: 0.0005% or more and 0.0050% or less.


Advantageous Effect

According to the disclosure, it becomes possible to manufacture a high-strength steel sheet having a tensile strength (TS) of 780 MPa or more and excellent in ductility, stretch flangeability, and fatigue properties with high productivity.


Also, a high-strength steel sheet manufactured by the method according to the disclosure is highly beneficial in industrial terms, because it can improve fuel efficiency when applied to, e.g., automobile structural members by a reduction in the weight of automotive bodies.







DETAILED DESCRIPTION

The present invention will be specifically described below.


According to the method disclosed herein, a steel slab with a predetermined chemical composition is heated and hot rolled. At this point, it is important to keep the mean coiling temperature (CT) during hot rolling low so that the hot-rolled steel sheet is provided with a structure in which a single phase structure of martensite, a single phase structure of bainite, or a martensite-bainite mixed structure is dominantly present.


It is also important when cold rolling is performed after hot rolling to set as low a rolling reduction as possible so that the resulting structure of the hot-rolled steel sheet will remain intact as much as possible.


In this way, a single phase structure of martensite, a single phase structure of bainite, or a martensite-bainite mixed structure is dominantly present in the structure of the steel sheet before subjection to annealing treatment. Consequently, even when annealing treatment is performed just once at a ferrite-austenite dual phase region, it becomes possible to form a structure that contains appropriate amounts of ferrite, bainitic ferrite, and retained austenite, and in which fine retained austenite and fine bainitic ferrite are distributed.


In addition, by causing the cooling stop temperature after annealing to drop to 350° C. or lower and performing reheating treatment under proper conditions, the structure may contain an appropriate amount of tempered martensite.


As a result, it becomes possible to manufacture a high-strength steel sheet having a tensile strength (TS) of 780 MPa or more and excellent in ductility, stretch flangeability, and fatigue properties with high productivity.


Firstly, the reasons for the limitations on the chemical composition of the steel manufactured according to our methods are described.


When components are expressed in “%,” this refers to “mass %” unless otherwise specified.


C: 0.10% or More and 0.35% or Less


C is an element that is important for increasing the strength of steel, has a high solid solution strengthening ability, and is essential for guaranteeing the presence of a desired amount of retained austenite to improve ductility.


If the C content is below 0.10%, it becomes difficult to obtain the required amount of retained austenite. If the C content exceeds 0.35%, however, the steel sheet is made brittle or susceptible to delayed fracture.


Therefore, the C content is 0.10% or more and 0.35% or less, preferably 0.15% or more and 0.30% or less, and more preferably 0.18% or more and 0.26% or less.


Si: 0.50% or More and 2.50% or Less


Si is an element that is effective in suppressing decomposition of retained austenite to carbides. Si also exhibits a high solid solution strengthening ability in ferrite, and has the property of purifying ferrite by facilitating solute C diffusion from ferrite to austenite to improve ductility. Moreover, Si dissolved in ferrite improves strain hardenability and increases the ductility of ferrite itself. To obtain this effect, the Si content needs to be 0.50% or more. If the Si content exceeds 2.50%, however, an abnormal structure grows, causing ductility to deteriorate.


Therefore, the Si content is 0.50% or more and 2.50% or less, preferably 0.80% or more and 2.00% or less, and more preferably 1.20% or more and 1.80% or less.


Mn: 2.00% or More and Less than 3.50%


Mn is effective in guaranteeing strength. Mn also improves hardenability to facilitate formation of a multi-phase structure. Moreover, Mn acts to suppress formation of ferrite and pearlite during a cooling process after hot rolling, and thus is an effective element in causing the hot-rolled sheet to have a structure in which a low temperature transformation phase (bainite or martensite) is dominantly present. To obtain this effect, the Mn content needs to be 2.00% or more. If the Mn content is 3.50% or more, however, Mn segregation becomes significant in the sheet thickness direction, leading to deterioration of fatigue properties.


Therefore, the Mn content is 2.00% or more and less than 3.50%, preferably 2.00% or more and 3.00% or less, and more preferably 2.00% or more and 2.80% or less.


P: 0.001% or More and 0.100% or Less


P is an element that has a solid solution strengthening effect and can be added depending on a desired strength. P also facilitates transformation to ferrite, and thus is an effective element in forming a multi-phase structure. To obtain this effect, the P content needs to be 0.001% or more. If the P content exceeds 0.100%, however, weldability degrades and, when a galvanized layer is subjected to alloying treatment, the alloying rate decreases, impairing galvanizing quality.


Therefore, the P content is 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 to grain boundaries, makes the steel brittle during hot working, and forms sulfides to reduce local deformability. Therefore, the S content needs to be 0.0200% or less. Under manufacturing constraints, however, the S content is necessarily 0.0001% or more.


Therefore, the S content is 0.0001% or more and 0.0200% or less, and preferably 0.0001% or more and 0.0050% or less.


N: 0.0005% or More and 0.0100% or Less


N is an element that deteriorates the anti-aging property of steel. Deterioration of the anti-aging property becomes more pronounced, particularly when the N content exceeds 0.0100%. Under manufacturing constraints, the N content is necessarily 0.0005% or more, although smaller N contents are more preferable.


Therefore, the N content is 0.0005% or more and 0.0100% or less, and preferably 0.0005% or more and 0.0070% or less.


In addition to the above basic components, at least one element selected from the group consisting of Ti and B may also be included. In particular, when the steel contains both Ti and B in appropriate amounts, the resulting hot-rolled sheet may be provided more advantageously with a structure in which a single phase structure of martensite, a single phase structure of bainite, or a martensite-bainite mixed structure is dominantly present.


Ti: 0.005% or More and 0.100% or Less


Ti forms fine precipitates during hot rolling or annealing to increase strength. In addition, Ti precipitates as TiN with N, and may thus suppress precipitation of BN when B is added to the steel, thereby effectively bringing out the effect of B as described below. To obtain this effect, the Ti content needs to be 0.005% or more. If the Ti content exceeds 0.100%, however, strengthening by precipitation works excessively, leading to deterioration of ductility. Therefore, the Ti content is preferably 0.005% or more and 0.100% or less, and more preferably 0.010% or more and 0.080% or less.


B: 0.0001% or More and 0.0050% or Less


B has the effect of suppressing ferrite-pearlite transformation during a cooling process after hot rolling so that the hot-rolled sheet has a structure in which a low temperature transformation phase (bainite or martensite), in particular martensite is dominantly present. B is also effective in increasing the strength of steel. To obtain this effect, the B content needs to be 0.0001% or more. However, excessively adding B beyond 0.0050% forms excessive martensite, raising a concern that ductility might decrease due to a rise in strength.


Therefore, the B content is preferably 0.0001% or more and 0.0050% or less, and more preferably 0.0005% or more and 0.0030% or less.


Mn Content/B Content: 2100 or Less


In particular for a low-Mn chemical composition, ferrite-pearlite transformation develops during a cooling process after hot rolling, which tends to cause ferrite and/or pearlite to be present in the structure of the hot-rolled sheet. As such, to bring out the above-described addition effect of B sufficiently, it is preferred that the Mn content divided by the B content (Mn content/B content) equals 2100 or less, and more preferably 2000 or less. No lower limit is particularly placed on the Mn content/B content, yet a preferred lower limit is approximately 300.


In addition to the above components, at least one element selected from the group consisting of the following may also be included:


Al: 0.01% or more and 1.00% or less, Nb: 0.005% or more and 0.100% or less, Cr: 0.05% or more and 1.00% or less, Cu: 0.05% or more and 1.00% or less, Sb: 0.002% or more and 0.200% or less, Sn: 0.002% or more and 0.200% or less, Ta: 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, and REM: 0.0005% or more and 0.0050% or less.


Al: 0.01% or More and 1.00% or Less


Al is an element that is effective in forming ferrite and improving the balance between strength and ductility. To obtain this effect, the Al content needs to be 0.01% or more. On the other hand, an Al content exceeding 1.00% leads to deterioration of surface characteristics.


Therefore, when Al is added to steel, the Al content is 0.01% or more and 1.00% or less, and preferably 0.03% or more and 0.50% or less.


Nb: 0.005% or More and 0.100% or Less


Nb forms fine precipitates during hot rolling or annealing to increase strength. To obtain this effect, the Nb content needs to be 0.005% or more. If the Nb content exceeds 0.100%, however, formability deteriorates.


Therefore, when Nb is added to steel, the Nb content is 0.005% or more and 0.100% or less.


Cr: 0.05% or More and 1.00% or Less, Cu: 0.05% or More and 1.00% or Less


Cr and Cu not only serve as solid-solution-strengthening elements, but also act to stabilize austenite in a cooling process during annealing, facilitating formation of a multi-phase structure. To obtain this effect, the Cr and Cu contents each need to be 0.05% or more. If the Cr and Cu contents both exceed 1.00%, formability deteriorates.


Therefore, when Cr and Cu are added to steel, respective contents are 0.05% or more and 1.00% or less.


Sb: 0.002% or More and 0.200% or Less, Sn: 0.002% or More and 0.200% or Less


Sb and Sn may be added as necessary for suppressing decarbonization of a region extending from the surface layer of the steel sheet to a depth of about several tens of micrometers, which is caused by nitriding and/or oxidation of the steel sheet surface. Suppressing such nitriding or oxidation is effective in preventing a reduction in the amount of martensite formed in the steel sheet surface and guaranteeing strength. To obtain this effect, the Sb and Sn contents each need to be 0.002% or more. However, excessively adding any of these elements beyond 0.200% leads to deterioration of toughness. Therefore, when Sb and Sn are added to steel, respective contents are 0.002% or more and 0.200% or less.


Ta: 0.001% or More and 0.100% or Less


As is the case with Ti and Nb, Ta forms alloy carbides or alloy carbonitrides, and contributes to increasing the strength of steel. It is also believed that Ta has the effect of significantly suppressing coarsening of precipitates when partially dissolved in Nb carbides or Nb carbonitrides to form complex precipitates, such as (Nb, Ta) (C, N), and providing a stable contribution to increasing strength through strengthening by precipitation. This precipitate-stabilizing effect can be obtained when the Ta content is 0.001% or more. However, excessively adding Ta beyond 0.100% fails to further increase the precipitate-stabilizing effect, but instead increases alloy costs. Therefore, when Ta is added to steel, the Ta content is 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, REM: 0.0005% or More and 0.0050% or Less


Ca, Mg, and REM are elements that are used for deoxidation, and are effective in causing spheroidization of sulfides and mitigating the adverse effect of sulfides on local ductility and stretch flangeability. To obtain this effect, Ca, Mg, and REM each need to be added to steel in an amount of 0.0005% or more. However, excessively adding Ca, Mg, and REM beyond 0.0050% leads to increased inclusions and the like, causing defects on the steel sheet surface and internal defects.


Therefore, when Ca, Mg, and REM are added to steel, respective contents are 0.0005% or more and 0.0050% or less.


The balance other than the above components consists of Fe and incidental impurities.


The following provides a description of manufacturing conditions in the method according to the disclosure.


The method for manufacturing a high-strength steel sheet according to the disclosure comprises: preparing a steel slab with the aforementioned chemical composition; subjecting the steel slab to hot rolling by heating the steel slab to a temperature of 1100° C. or higher and 1300° C. or lower, hot rolling the steel slab with a finisher delivery temperature of 800° C. or higher and 1000° C. or lower to form a hot-rolled steel sheet, and coiling the hot-rolled steel sheet at a mean coiling temperature of 200° C. or higher and 500° C. or lower; subjecting the hot-rolled steel sheet to pickling treatment; optionally cold rolling the hot-rolled steel sheet at a rolling reduction below 30% to form a cold-rolled steel sheet; subjecting the hot-rolled or cold-rolled steel sheet to annealing by retaining the steel sheet at a temperature of 740° C. or higher and 840° C. or lower for 10 s or more and 900 s or less, and then cooling the steel sheet at a mean cooling rate of 5° C./s or higher and 30° C./s or lower to a cooling stop temperature of 150° C. or higher and 350° C. or lower; and subsequently subjecting the hot-rolled or cold-rolled steel sheet to reheating treatment by reheating the steel sheet to a reheating temperature of higher than 350° C. and 550° C. or lower, and retaining the steel sheet at the reheating temperature for 10 s or more.


In the above steps, the temperatures, such as the finisher delivery temperature, the mean coiling temperature, and the like, all represent temperatures measured at the steel sheet surface. The mean cooling rate is also calculated from temperatures measured at the steel sheet surface.


The following explains the reasons for the limitations placed on the manufacturing conditions.


Steel Slab Heating Temperature: 1100° C. or Higher and 1300° C. or Lower


Precipitates that are present at the time of heating of a steel slab will remain as coarse precipitates in the resulting steel sheet, making no contribution to strength. Thus, remelting of any Ti- and Nb-based precipitates precipitated during casting is required.


In this respect, if a steel slab is heated at a temperature below 1100° C., it is difficult to cause sufficient melting of carbides, leading to problems such as an increased risk of trouble during hot rolling resulting from increased rolling load. In addition, for obtaining a smooth steel sheet surface, it is necessary to scale-off defects on the surface layer of the slab, such as blow hole generation, segregation, and the like, and to reduce cracks and irregularities on the steel sheet surface. Therefore, the steel slab heating temperature needs to be 1100° C. or higher.


If the steel slab heating temperature exceeds 1300° C., however, scale loss increases as oxidation progresses. Therefore, the steel slab heating temperature needs to be 1300° C. or lower.


For this reason, the steel slab heating temperature is 1100° C. or higher and 1300° C. or lower, and preferably 1150° C. or higher and 1250° C. or lower.


A steel slab is preferably made with continuous casting to prevent macro segregation, yet may be produced with other methods such as ingot casting or thin slab casting. The steel slab thus produced may be cooled to room temperature and then heated again according to the conventional method. Alternatively, there can be employed without problems what is called “energy-saving” processes, such as hot direct rolling or direct rolling in which either a warm steel slab without being fully cooled to room temperature is charged into a heating furnace, or a steel slab undergoes heat retaining for a short period and immediately hot rolled. Further, a steel slab is subjected to rough rolling under normal conditions and formed into a sheet bar. When the heating temperature is low, the sheet bar is preferably heated using a bar heater or the like prior to finish rolling from the viewpoint of preventing troubles during hot rolling.


Finisher Delivery Temperature in Hot Rolling: 800° C. or Higher and 1000° C. or Lower


The heated steel slab is hot rolled through rough rolling and finish rolling to form a hot-rolled steel sheet. At this point, when the finisher delivery temperature exceeds 1000° C., the amount of oxides (scales) generated suddenly increases and the interface between the steel substrate and oxides becomes rough, which tends to impair the surface quality after pickling and cold rolling. In addition, any hot-rolling scales remaining after pickling adversely affect ductility. Further, grain size increases excessively and fatigue properties deteriorate.


On the other hand, if the finisher delivery temperature is below 800° C., rolling load and burden increase, rolling is performed more often in a state in which recrystallization of austenite does not occur, and an abnormal texture develops. As a result, the final product has a significant planar anisotropy, and not only does the material properties become less uniform, but also the ductility itself deteriorate.


Therefore, the finisher delivery temperature in hot rolling needs to be 800° C. or higher and 1000° C. or lower, and preferably 820° C. or higher and 950° C. or lower.


Mean Coiling Temperature after Hot Rolling: 200° C. or Higher and 500° C. or Lower


Setting of mean coiling temperature after the hot rolling is very important for the method according to the disclosure.


Specifically, when the mean coiling temperature after the hot rolling is above 500° C., ferrite and pearlite form during cooling and retaining processes after the hot rolling. Consequently, it becomes difficult to provide the hot-rolled sheet with a structure in which a single phase structure of martensite, a single phase structure of bainite, or a martensite-bainite mixed structure is dominantly present, making it difficult to impart a desired ductility to the steel sheet obtained after annealing or to balance its strength and ductility. If the mean coiling temperature after the hot rolling is below 200° C., the hot-rolled steel sheet is degraded in terms of shape, deteriorating productivity. Therefore, the mean coiling temperature after the hot rolling needs to be 200° C. or higher and 500° C. or lower, preferably 300° C. or higher and 450° C. or lower, and more preferably 350° C. or higher and 450° C. or lower.


Finish rolling may be performed continuously by joining rough-rolled sheets during the hot rolling. Rough-rolled sheets may be coiled on a temporary basis. At least part of finish rolling may be conducted as lubrication rolling to reduce rolling load in hot rolling. Conducting lubrication rolling in such a manner is effective from the perspective of making the shape and material properties of a steel sheet uniform. In lubrication rolling, the coefficient of friction is preferably 0.10 or more and 0.25 or less.


The hot-rolled steel sheet thus produced is subjected to pickling. Pickling enables removal of oxides from the steel sheet surface, and is thus important to ensure that the high-strength steel sheet as the final product has good chemical convertibility and a sufficient quality of coating. Pickling may be performed in one or more batches.


Rolling Reduction in Cold Rolling: Less than 30%


Additionally, the hot-rolled steel sheet may be subjected to cold rolling to form a cold-rolled steel sheet. When cold rolling is performed, rolling reduction in cold rolling is of great importance.


Specifically, if the rolling reduction is 30% or more, a low temperature transformation phase is broken in the structure of the hot-rolled sheet. Consequently, it becomes difficult to provide the steel sheet obtained after the annealing with a structure that contains appropriate amounts of ferrite, bainitic ferrite, and retained austenite, and in which fine retained austenite and fine bainitic ferrite are distributed, making it difficult to ensure ductility, balance strength and ductility, or guarantee good fatigue properties.


Therefore, the rolling reduction in cold rolling is less than 30%, preferably 25% or less, and more preferably 20% or less. No lower limit is particularly placed on the rolling reduction in cold rolling. It may be greater than 0%. The number of rolling passes and the rolling reduction per pass are not particularly limited, and the effect of the disclosure may be obtained with any number of rolling passes and any rolling reduction per pass.


Annealing Temperature: 740° C. or Higher and 840° C. or Lower


An annealing temperature below 740° C. cannot ensure formation of a sufficient amount of austenite during the annealing. Consequently, a desired amount of retained austenite cannot be obtained in the end, making it difficult to yield good ductility and to balance strength and ductility. On the other hand, an annealing temperature above 840° C. is within a temperature range of austenite single phase, and a desired amount of fine retained austenite cannot be produced in the end, which makes it difficult again to ensure good ductility and to balance strength and ductility.


Therefore, the annealing temperature is 740° C. or higher and 840° C. or lower, and preferably 750° C. or higher and 830° C. or lower.


Annealing Treatment Holding Time: 10 s or More and 900 s or Less


A annealing treatment holding time shorter than 10 s cannot ensure formation of a sufficient amount of austenite during the annealing. Consequently, a desired amount of retained austenite cannot be obtained in the end, making it difficult to yield good ductility and to balance strength and ductility. On the other hand, an annealing treatment holding time longer than 900 s causes grain coarsening, a desired amount of fine retained austenite cannot be produced in the end, making it difficult to ensure good ductility and to balance strength and ductility. This also inhibits productivity.


Therefore, the annealing treatment holding time is 10 s or more and 900 s or less, preferably 30 s or more and 750 s or less, and more preferably 60 s or more and 600 s or less.


Mean Cooling Rate to a Cooling Stop Temperature of 150° C. or Higher and 350° C. or Lower: 5° C./s or Higher and 30° C./s or Lower


If the mean cooling rate to a cooling stop temperature of 150° C. or higher and 350° C. or lower is below 5° C./s, a large amount of ferrite is produced during cooling, making it difficult to guarantee a desired strength. On the other hand, if the mean cooling rate is above 30° C./s, a low temperature transformation phase forms excessively, degrading ductility.


Therefore, the mean cooling rate to a cooling stop temperature of 150° C. or higher and 350° C. or lower is 5° C./s or higher and 30° C./s or lower, and preferably 10° C./s or higher and 30° C./s or lower.


The cooling in the annealing is preferably performed by gas cooling; however, furnace cooling, mist cooling, roll cooling, water cooling, and the like can also be employed in combination.


In addition, if the cooling stop temperature is above 350° C., it is higher than the martensite transformation starting temperature (Ms), with the result that tempered martensite is not produced when reheating treatment is performed subsequently, hard and fresh martensite (martensite not tempered) remains in the resulting structure, and hole expansion formability (stretch flangeability) ends up deteriorating. On the other hand, if the cooling stop temperature is below 150° C., austenite transforms to martensite in a large amount, and a desired amount of retained austenite cannot be obtained in the end, making it difficult to obtain good ductility and to balance strength and ductility.


Therefore, the cooling stop temperature is 150° C. or higher and 350° C. or lower, and preferably 180° C. or higher and 320° C. or lower.


Reheating Temperature: Higher than 350° C. and 550° C. or Lower


If the reheating temperature is above 550° C., decomposition of retained austenite occurs, and a desired amount of retained austenite cannot be obtained in the end, making it difficult to yield good ductility and balance strength and ductility. On the other hand, if the heating temperature is 350° C. or lower, a desired amount of tempered martensite cannot be obtained, making it difficult to ensure hole expansion formability (stretch flangeability).


Therefore, the reheating temperature is higher than 350° C. and 550° C. or lower, and preferably 370° C. or higher and 530° C. or lower.


Holding Time at Reheating Temperature: 10 s or More


If the holding time at the reheating temperature is shorter than 10 s, there is insufficient time for the concentration of C (carbon) into austenite to progress, making it difficult to ensure a desired amount of retained austenite in the end. Therefore, the holding time at the reheating temperature is 10 s or more. However, a holding time longer than 600 s does not increase the amount of retained austenite and ductility does not significantly improve, where the effect reaches a plateau. Therefore, the holding time at the reheating temperature is preferably 600 s or less, more preferably 30 s or more and 500 s or less, and still more preferably 60 s or more and 400 s or less.


Cooling after the holding is not particularly limited, and any method may be used to implement cooling to a desired temperature.


The steel sheet thus obtained may be subjected to galvanizing treatment such as hot-dip galvanizing.


For example, when hot-dip galvanizing is performed, the above-described steel sheet subjected to the annealing treatment is immersed in a galvanizing bath at 440° C. or higher and 500° C. or lower for hot-dip galvanizing, after which coating weight adjustment is performed using gas wiping or the like. For hot-dip galvanizing, a galvanizing bath with an Al content of 0.10% or more and 0.22% or less is preferably used. When a galvanized layer is subjected to alloying treatment, the alloying treatment is performed in a temperature range of 470° C. to 600° C. after hot-dip galvanizing. If alloying treatment is performed at a temperature above 600° C., untransformed austenite transforms to pearlite, where the presence of a desired volume fraction of retained austenite cannot be ensured and ductility may degrade. Therefore, when a galvanized layer is subjected to alloying treatment, the alloying treatment is preferably performed in a temperature range of 470° C. to 600° C. Electrogalvanized plating may also be performed.


Moreover, when skin pass rolling is performed after the heat treatment, the skin pass rolling is preferably performed with a rolling reduction of 0.1% or more and 1.0% or less. A rolling reduction below 0.1% provides only a small effect and complicates control, and hence 0.1% is the lower limit of the favorable range. On the other hand, a rolling reduction above 1.0% significantly degrades productivity, and thus 1.0% is the upper limit of the favorable range.


The skin pass rolling may be performed on-line or off-line. Skin pass may be performed in one or more batches with a target rolling reduction. No particular limitations are placed on other manufacturing conditions, yet from the perspective of productivity, the aforementioned series of processes such as annealing, hot-dip galvanizing, and alloying treatment on a galvanized layer are preferably carried out on a CGL (Continuous Galvanizing Line) as the hot-dip galvanizing line. After the hot-dip galvanizing, wiping may be performed for adjusting the coating amounts.


The following describes the microstructure of a steel sheet manufactured by the method according to the disclosure.


Total Area Ratio of Ferrite and Bainitic Ferrite: 30% or More and 75% or Less

A high-strength steel sheet manufactured by the method according to the disclosure comprises a multi-phase structure in which retained austenite having an influence mainly on ductility and, more preferably, a small amount of martensite affecting strength are diffused in a structure in which soft ferrite with high ductility is dominantly present. In addition, bainitic ferrite forms adjacent to ferrite and retained austenite/martensite, and reduces the difference in hardness between ferrite and retained austenite and between ferrite and martensite to suppress the occurrence of cracking during hole expansion test and of fatigue cracking during fatigue test.


To ensure sufficient ductility, the total area ratio of ferrite and bainitic ferrite needs to be 30% or more. On the other hand, to secure strength, the total area ratio of ferrite and bainitic ferrite needs to be 75% or less. For better ductility, the total area ratio of ferrite and bainitic ferrite is preferably 35% or more and 70% or less.


Bainitic ferrite is effective in ensuring better hole expansion formability and better fatigue properties since, as described above, it forms adjacent to ferrite and retained austenite/martensite and has the effect of reducing the difference in hardness between ferrite and retained austenite and between ferrite and martensite to suppress the occurrence of cracking during hole expansion test and of fatigue cracking during fatigue test. Therefore, the area ratio of bainitic ferrite is preferably 5% or more. On the other hand, to secure stable strength, the area ratio of bainitic ferrite is preferably 25% or less.


As used herein, the term “bainitic ferrite” means such ferrite that is produced during the process of annealing at a temperature of 740° C. or higher and 840° C. or lower, followed by cooling to and holding at a temperature of 600° C. or lower, and that has a high dislocation density as compared to normal ferrite.


While the main example of ferrite is acicular ferrite, ferrite may include polygonal ferrite and non-recrystallized ferrite. To ensure good ductility, however, it is preferred that the area ratio of polygonal ferrite is 20% or less and the area ratio of non-recrystallized ferrite is 5% or less. The area ratios of polygonal ferrite and of non-recrystallized ferrite may be 0%.


The area ratios of ferrite and bainitic ferrite can be determined by polishing a cross section of a steel sheet taken in the sheet thickness direction to be parallel to the rolling direction (L-cross section), etching the cross section with 3 vol. % nital, and averaging the results from observing ten locations at 2000 times magnification under an SEM (scanning electron microscope) at a position of sheet thickness×¼ (a position at a depth of one-fourth of the sheet thickness from the steel sheet surface) and calculating the area ratios of ferrite and bainitic ferrite for the ten locations with Image-Pro, available from Media Cybernetics, Inc., using the structure micrographs imaged with the SEM.


In the structure micrographs, ferrite and bainitic ferrite appear as a gray structure (base steel structure), while retained austenite and martensite as a white structure.


Identification of ferrite and bainitic ferrite is made by EBSD (Electron Back Scatter Diffraction) measurement. Specifically, a crystal grain (phase) that includes a sub-boundary with a grain boundary angle of smaller than 15° is identified as bainitic ferrite, for which the area ratio is calculated and used as the area ratio of bainitic ferrite. The area ratio of ferrite can be calculated by subtracting the area ratio of bainitic ferrite from the area ratio of the above-described gray structure.


Area Ratio of Tempered Martensite: 5% or More and 15% or Less


To ensure good hole expansion formability (stretch flangeability), the area ratio of tempered martensite needs to be 5% or more. For better hole expansion formability (stretch flangeability), it is preferred that the area ratio of tempered martensite is 8% or more. If the area ratio of tempered martensite exceeds 15%, however, it becomes difficult to obtain a sufficient amount of retained austenite. This results in a difficulty in obtaining good ductility and balancing strength and ductility. Therefore, the area ratio of tempered martensite needs to be 15% or less.


Here, tempered martensite can be identified by determining whether cementite or retained austenite is included in martensite (tempered martensite is martensite containing cementite or retained austenite). The area ratio of tempered martensite can be determined by polishing an L-cross section of a steel sheet, etching the cross section with 3 vol. % nital, and averaging the results from observing ten locations at 2000 times magnification under an SEM (scanning electron microscope) at a position of sheet thickness×¼ and calculating the area ratios of ferrite and bainitic ferrite for the ten locations with Image-Pro, available from Media Cybernetics, Inc., using the structure micrographs imaged with the SEM.


Volume Fraction of Retained Austenite: 8% or More


To ensure good ductility and balance strength and ductility, the volume fraction of retained austenite needs to be 8% or more. For obtaining better ductility and achieving a better balance between strength and ductility, it is preferred that the volume fraction of retained austenite is 10% or more. No upper limit is particularly placed on the volume fraction of retained austenite, yet it is around 35%.


The volume fraction of retained austenite is calculated by determining the x-ray diffraction intensity of a plane of sheet thickness×¼, which is exposed by polishing the steel sheet surface to a depth of one-fourth of the sheet thickness. Using an incident x-ray beam of MoKα, the intensity ratio of the peak integrated intensity of the {111}, {200}, {220}, and {311} planes of retained austenite to the peak integrated intensity of the {110}, {200}, and {211} planes of ferrite is calculated for all of the twelve combinations, the results are averaged, and the average is used as the volume fraction of retained austenite.


Mean Grain Size of Retained Austenite: 2 μm or Less


Refinement of retained austenite grains contributes to improving the ductility and fatigue properties of the steel sheet. Accordingly, to ensure good ductility and fatigue properties, retained austenite needs to have a mean grain size of 2 μm or less. For better ductility and fatigue properties, it is preferred that retained austenite has a mean grain size of 1.5 μm or less. No lower limit is particularly placed on the mean grain size, yet it is around 0.1 μm.


The mean grain size of retained austenite can be determined by averaging the results from observing twenty locations at 15000 times magnification under a TEM (transmission electron microscope) and averaging the equivalent circular diameters calculated from the areas of retained austenite grains identified with Image-Pro, as mentioned above, using the structure micrographs imaged with the TEM.


Mean Free Path of Bainitic Ferrite: 3 μm or Less


The mean free path of bainitic ferrite is very important. Specifically, bainitic ferrite forms in the process of cooling to and holding at a temperature of 600° C. or lower following the annealing in a temperature range of 740° C. to 840° C. In this respect, bainitic ferrite forms adjacent to ferrite and retained austenite, and has the effect of reducing the difference in hardness between ferrite and retained austenite to suppress the occurrence of fatigue cracking and propagation of cracking. It is thus more advantageous if bainitic ferrite is densely distributed, in other words, if bainitic ferrite has a small mean free path.


To ensure good fatigue properties, bainitic ferrite needs to have a mean free path of 3 μm or less. For better fatigue properties, it is preferred that bainitic ferrite has a mean free path of 2.5 μm or less. No lower limit is particularly placed on the mean free path, yet it is around 0.5 μm.


The mean free path (LBF) of bainitic ferrite can be calculated by:







L
BF

=




d
BF

2




(


4

π


3





f


)


1
3



-

d
BF






LBF: mean free path of bainitic ferrite (μm)


dBF: mean grain size of bainitic ferrite (μm)


f: area ratio of bainitic ferrite (%)÷100


The mean grain size of bainitic ferrite can be determined by averaging the areas of grains by dividing the area of bainitic ferrite in the measured region calculated by EBSD (Electron Back Scatter Diffraction) measurement by the number of bainitic ferrite grains in the measured region to identify an equivalent circle diameter.


In addition to ferrite and bainitic ferrite, tempered martensite, and retained austenite, the microstructures according to the disclosure may include carbides such as martensite, pearlite, cementite, and the like, as well as other microstructures well known as steel sheet microstructures. Any microstructure that has an area ratio of 15% or less may be used without detracting from the effect of the disclosure.


Examples

Steels having the chemical compositions presented in Table 1, each with the balance consisting of Fe and incidental impurities, were prepared by steelmaking in a converter and formed into slabs by continuous casting. The steel slabs thus obtained were heated under the conditions presented in Table 2, and subjected to hot rolling, followed by pickling treatment. For Steel Nos. 1, 3-6, 8, 9, 12, 14, 16-19, 21, 24, 26, 29, 31, 33, 35, 37, 38, 40, 42, 43, 47, 50, 51, 53, 56, and 60 presented in Table 2, cold rolling was not performed, and annealing treatment was conducted under the conditions presented in Table 2 to produce high-strength hot-rolled steel sheets (HR). For Steel Nos. 2, 7, 10, 11, 13, 15, 20, 22, 23, 25, 27, 28, 30, 32, 34, 36, 39, 41, 44-46, 48, 49, 52, 54, 55, 57-59, and 61 presented in Table 2, cold rolling was performed, and annealing treatment was conducted under the conditions presented in Table 2 to produce high-strength cold-rolled steel sheets (CR). Moreover, some were subjected to galvanizing treatment to obtain hot-dip galvanized steel sheets (GI), galvannealed steel sheets (GA), and electrogalvanized steel sheets (EG).


Used as hot-dip galvanizing baths were a zinc bath containing 0.19 mass % of Al for GI and a zinc bath containing 0.14 mass % of Al for GA, in each case the bath temperature was 465° C. The coating weight per side was 45 g/m2 (in the case of both-sided coating), and the Fe concentration in the coated layer of each hot-dip galvannealed steel sheet (GA) was 9 mass % or more and 12 mass % or less.


The Ac1 transformation temperature (° C.) presented in Table 1 was calculated by:





Ac1 transformation temperature (° C.)=751−16×(% C)+11×(% Si)−28×(% Mn)−5.5×(% Cu)+13×(% Cr)

    • Where (% X) represents content (in mass %) of an element X in steel.





























TABLE 1


























Ac1






















transformation












Chemical composition (mass %)
temperature




























Steel ID
C
Si
Mn
P
S
N
B
Ti
Al
Nb
Cr
Cu
Sb
Sn
Ta
Ca
Mg
REM
(° C.)
Remarks





A
0.112
1.62
2.38
0.021
0.0020
0.0032












700
Conforming steel


B
0.182
1.24
2.11
0.019
0.0019
0.0030












703
Conforming steel


C
0.211
1.28
2.14
0.014
0.0018
0.0032












705
Conforming steel


D
0.232
0.73
2.34
0.025
0.0022
0.0030












690
Conforming steel


E
0.224
1.02
2.13
0.029
0.0016
0.0032












702
Conforming steel


F
0.218
1.48
2.09
0.016
0.0024
0.0033












709
Conforming steel


G
0.228
1.55
2.16
0.018
0.0019
0.0034












704
Conforming steel


H
0.200
1.48
2.34
0.022
0.0021
0.0030












699
Conforming steel


I
0.182
1.39
2.86
0.028
0.0019
0.0029












683
Conforming steel


J

0.064

1.51
2.89
0.027
0.0018
0.0028












686
Comparative steel


K
0.232

0.24

2.78
0.023
0.0021
0.0030












672
Comparative steel


L
0.213
1.43

1.72

0.028
0.0028
0.0028












715
Comparative steel


M
0.202
1.34
2.22
0.018
0.0024
0.0034


0.380









700
Conforming steel


N
0.198
1.22
2.11
0.031
0.0022
0.0031

0.034










707
Conforming steel


O
0.188
1.24
2.25
0.016
0.0026
0.0032



0.041








709
Conforming steel


P
0.234
1.48
2.41
0.028
0.0018
0.0030




0.22







712
Conforming steel


Q
0.203
1.46
2.21
0.015
0.0024
0.0029





0.25






701
Conforming steel


R
0.221
1.49
2.18
0.024
0.0019
0.0033






0.0051





703
Conforming steel


S
0.187
1.56
2.34
0.019
0.0028
0.0034







0.0046




710
Conforming steel


T
0.189
1.45
2.03
0.024
0.0018
0.0029








0.0039



707
Conforming steel


U
0.199
1.32
2.09
0.025
0.0017
0.0044



0.041


0.0060





704
Conforming steel


V
0.202
1.38
2.12
0.018
0.0026
0.0036



0.020



0.0062




704
Conforming steel


W
0.211
1.46
2.28
0.028
0.0025
0.0042



0.034




0.0055



709
Conforming steel


X
0.213
1.24
2.42
0.019
0.0022
0.0044









0.0024


707
Conforming steel


Y
0.197
1.44
2.21
0.024
0.0019
0.0036










0.0016

702
Conforming steel


Z
0.198
1.63
2.09
0.020
0.0017
0.0032











0.0020
707
Conforming steel


AA
0.178
1.42
2.30
0.012
0.0015
0.0033
0.0019
0.021










699
Conforming steel


AB
0.252
1.01
2.11
0.018
0.0022
0.0041
0.0012
0.018










699
Conforming steel


AC
0.181
1.49
2.61
0.019
0.0021
0.0032
0.0011
0.023










691
Conforming steel


AD
0.143
0.98
2.79
0.012
0.0016
0.0035
0.0026
0.032










681
Conforming steel


AE
0.112
1.39
2.33
0.021
0.0024
0.0039
0.0021
0.026










699
Conforming steel


AF
0.109
1.21
2.18
0.019
0.0021
0.0033












702
Conforming steel


AG
0.115
1.30
2.86
0.028
0.0019
0.0034
0.0030
0.018










683
Conforming steel


AH
0.113
0.89
2.12
0.015
0.0018
0.0030












700
Conforming steel


AI
0.126
0.97
2.83
0.024
0.0021
0.0029
0.0025
0.030










680
Conforming steel


AJ
0.121
2.30
2.89
0.019
0.0028
0.0028












693
Conforming steel


AK
0.308
1.22
2.10
0.024
0.0024
0.0030
0.0015
0.028










701
Conforming steel


AL
0.295
1.44
2.41
0.022
0.0022
0.0028












695
Conforming steel


AM
0.293
1.22
2.69
0.021
0.0026
0.0034
0.0035
0.015










684
Conforming steel


AN
0.131
1.33
2.38
0.022
0.0018
0.0037
0.0018
0.060










697
Conforming steel


AO
0.177
1.47
2.79
0.006
0.0024
0.0032












686
Conforming steel


AP
0.190
1.40
2.68
0.017
0.0007
0.0041
0.0020
0.025










688
Conforming steel


AQ
0.228
1.32
2.47
0.007
0.0006
0.0040












693
Conforming steel





Underlined if outside of the appropriate range.
























TABLE 2










Hot-rolling





Reheating treatment




















conditions
Cold-rolling
Annealing treatment conditions
conditions
























Slab
Finisher
Mean
conditions

Annealing
Mean
Cooling

Reheating






heating
delivery
coiling
Rolling
Annealing
holding
cooling
stop
Reheating
holding





Steel
temp.
temp.
temp.
reduction
temp.
time
rate
temp.
temp.
time




No.
ID
(° C.)
(° C.)
(° C.)
(%)
(° C.)
(s)
(° C./s)
(° C.)
(° C.)
(s)
Type*
Remarks























 1
A
1250
 910
400
cold rolling not
770
 120
17
220
400
190
HR
Example







performed










 2
B
1260
 890
440
13.0
790
 150
20
190
500
340
GI
Example


 3
C
1230
 870
410
cold rolling not
780
 140
22
200
420
210
HR
Example







performed










 4
C
890
 900
400
cold rolling not
810
 200
15
230
430
150
HR
Comparative







performed







example


 5
C

1420

 910
420
cold rolling not
800
 240
16
200
450
130
HR
Comparative







performed







example


 6
C
1220
640
380
cold rolling not
810
 280
17
190
390
210
HR
Comparative







performed







example


 7
C
1230

1120

490
 6.0
800
 180
17
220
400
290
CR
Comparative















example


 8
C
1240
 910

120

cold rolling not
790
 300
18
240
400
210
GI
Comparative







performed







example


 9
C
1260
 890

630

cold rolling not
790
 250
22
250
420
230
HR
Comparative







performed







example


10
C
1230
 900
420

46.2

820
 200
17
280
500
240
CR
Comparative















example


11
C
1230
 920
450
13.0

660

 280
15
240
480
180
EG
Comparative















example


12
C
1220
 860
470
cold rolling not

900

 100
16
200
490
210
HR
Comparative







performed







example


13
C
1240
 870
460
 5.3
780
  5
17
170
460
290
CR
Comparative















example


14
C
1250
 900
480
cold rolling not
790

1200

17
300
440
260
HR
Comparative







performed







example


15
C
1260
 910
500
 8.7
800
 180

72

260
420
190
EG
Comparative















example


16
C
1250
 900
480
cold rolling not
810
 220
17
70
400
160
GI
Comparative







performed







example


17
C
1230
 860
460
cold rolling not
800
 240
15

550

450
170
HR
Comparative







performed







example


18
C
1240
 900
450
cold rolling not
810
 180
14
220

270

150
HR
Comparative







performed







example


19
C
1200
 870
420
cold rolling not
820
 150
12
200

620

200
HR
Comparative







performed







example


20
C
1230
 890
400
 8.0
810
 300
18
230
420
5
GA
Comparative















example


21
C
1240
 880
450
cold rolling not
790
 180
20
220
500
950
GI
Example







performed










22
D
1220
 890
460
11.1
770
 180
24
200
480
480
CR
Example


23
E
1230
 900
420
11.1
790
 200
24
240
380
260
CR
Example


24
F
1240
 910
480
cold rolling not
760
 240
22
220
400
270
GA
Example







performed










25
G
1230
 880
500
 6.3
790
 190
20
190
460
190
CR
Example


26
H
1220
 860
470
cold rolling not
760
 150
22
200
450
170
EG
Example







performed










27
I
1210
 880
490
 8.7
820
 100
19
220
480
150
CR
Example


28

J

1200
 860
500
 8.0
760
 180
22
240
430
190
CR
Comparative















example


29

K

1230
 890
470
cold rolling not
820
 150
17
230
400
510
EG
Comparative







performed







example


30

L

1230
 890
460
 4.3
800
 170
16
210
420
200
CR
Comparative















example


31
M
1250
 900
420
cold rolling not
820
 200
18
200
480
450
GI
Example







performed










32
N
1240
 890
450
 5.3
750
 90
16
210
500
510
CR
Example


33
O
1240
 880
460
cold rolling not
780
 120
27
220
450
180
HR
Example







performed










34
P
1250
 860
400
 5.6
790
 180
26
240
410
520
CR
Example


35
Q
1230
 890
440
cold rolling not
800
 80
17
190
400
400
EG
Example







performed










36
R
1220
 860
400
 5.3
800
 160
28
200
460
180
GA
Example


37
S
1230
 910
380
cold rolling not
790
 200
17
230
420
190
GI
Example







performed










38
T
1220
 880
410
cold rolling not
810
 240
17
240
410
380
EG
Example







performed










39
U
1230
 880
400
 5.3
790
 160
16
200
400
540
GI
Example


40
V
1240
 890
420
cold rolling not
800
 280
15
190
450
250
HR
Example







performed










41
W
1220
 880
400
 8.0
780
 200
16
180
420
180
EG
Example


42
X
1230
 910
350
cold rolling not
810
 90
22
260
400
200
HR
Example







performed










43
Y
1230
 870
380
cold rolling not
770
 150
20
240
460
180
GI
Example







performed










44
Z
1210
 860
400
 5.3
800
 200
20
200
450
190
CR
Example


45
AA
1250
 900
450
11.1
790
 200
15
200
410
200
CR
Example


46
AB
1220
 910
480
 9.1
800
 180
14
210
430
180
GA
Example


47
AC
1240
 870
490
cold rolling not
780
 250
13
180
410
200
HR
Example







performed










48
AD
1230
 880
480
10.0
810
 200
16
230
400
150
GI
Example


49
AE
1250
 900
400
11.1
820
 250
14
200
410
220
CR
Example


50
AF
1240
 880
440
cold rolling not
790
 180
22
240
380
180
HR
Example







performed










51
AG
1210
 890
400
cold rolling not
800
 200
18
220
400
150
HR
Example







performed










52
AH
1200
 900
380
12.5
820
 200
22
210
460
200
GA
Example


53
AI
1230
 910
410
cold rolling not
790
 250
19
200
450
150
HR
Example







performed










54
AJ
1230
 880
400
13.3
830
 230
21
200
450
190
EG
Example


55
AK
1240
 880
420
 6.3
790
 160
17
220
390
510
CR
Example


56
AL
1220
 890
400
cold rolling not
760
 300
16
210
400
200
HR
Example







performed










57
AM
1230
 880
350
 7.7
780
 170
17
190
400
450
CR
Example


58
AN
1230
 910
420
 6.7
800
 250
16
270
420
510
CR
Example


59
AO
1210
 860
380
 6.7
820
 90
26
190
500
190
CR
Example


60
AP
1230
 880
400
cold rolling not
810
 100
17
220
480
410
HR
Example







performed










61
AQ
1250
 900
420
 6.7
810
 200
18
210
400
350
GI
Example





Underlined if outside of the appropriate range.


*HR: Hot-rolled steel sheets (uncoated), CR: Cold-rolled steel sheets (uncoated),


GI: hot-dip galvanized steel sheets (alloying treatment not performed on galvanized layers),


GA: galvannealed steel sheets,


EG: electrogalvanized steel sheets






The high-strength hot-rolled steel sheets (HR), high-strength cold-rolled steel sheets (CR), hot-dip galvanizing steel sheets (GI), galvannealed steel sheets (GA), and electrogalvanized steel sheets (EG) thus obtained were subjected to structure observation, tensile test, hole expansion test, and fatigue test.


In this case, tensile test was performed in accordance with JIS Z 2241 (2011) to measure TS (tensile strength) and EL (total elongation), using JIS No. 5 test pieces that were sampled such that the longitudinal direction of each test piece coincides with a direction perpendicular to the rolling direction of the steel sheet (the C direction).


In this case, TS and EL were determined to be good when EL≧34% for TS 780 MPa grade, EL≧27% for TS 980 MPa grade, and EL≧23% for TS 1180 MPa grade, and TS×EL≧27000 MPa·%.


Further, hole expansion test was performed in accordance with JIS Z 2256 (2010). Each of the steel sheets thus obtained was cut to a sample size of 100 mm×100 mm, and a hole with a diameter of 10 mm was drilled through each sample with clearance 12%±1%. Subsequently, each steel sheet was clamped into a die having an inner diameter of 75 mm with a blank holding force of 8 tons (7.845 kN). In this state, a conical punch of 60° was pushed into the hole, and the hole diameter at the time of occurrence of cracking (hole diameter at crack initiation limit) was measured. Based on the hole diameter thus measured, the maximum hole expansion ratio λ (%) was calculated by the following equation to evaluate hole expansion formability:





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

    • Where Df is a hole diameter at the time of occurrence of cracking (mm) and D0 is an initial hole diameter (mm).


      In this case, TS and EL were determined to be good when λ≧40% for TS 780 MPa grade, λ≧30% for TS 980 MPa grade, and λ≧20% TS 1180 MPa grade.


Moreover, in fatigue test, sampling was performed such that the longitudinal direction of each fatigue test piece coincides with a direction perpendicular to the rolling direction of the steel sheet, and plane bending fatigue test was conducted under the completely reversed (stress ratio: −1) condition and at the frequency of 20 Hz in accordance with JIS Z 2275 (1978). In the completely reversed plane bending fatigue test, the stress at which no fracture was observed after 107 cycles was measured and used as fatigue limit strength.


Fatigue limit strength was divided by tensile strength TS to calculate a fatigue ratio. In this case, the fatigue property was determined to be good when fatigue limit strength ≧400 MPa and fatigue ratio ≧0.40.


Additionally, during the manufacture of steel sheets, measurements were made of productivity, sheet passage ability during hot rolling and cold rolling, and surface characteristics of each steel sheet obtained after final annealing (hereinafter also referred to as a “final-annealed sheet”).


In this case, productivity was evaluated according to the lead time costs, including:

    • (1) malformation of a hot-rolled steel sheet occurred;
    • (2) a hot-rolled steel sheet requires straightening before proceeding to the subsequent steps;
    • (3) a prolonged annealing treatment holding time; and
    • (4) a prolonged austemper holding time (a prolonged holding time in a reheating temperature range in annealing treatment).


      The productivity was determined to be “high” when none of (1) to (4) applied, “middle” when only (4) applied, and “low” when any of (1) to (3) applied.


The sheet passage ability during hot rolling was determined to be low when the risk of trouble during rolling increased with increasing rolling load. Similarly, the sheet passage ability during cold rolling was determined to be low when the risk of trouble during rolling increased with increasing rolling load.


Furthermore, the surface characteristics of each final-annealed sheet were determined to be poor when defects such as blow hole generation and segregation on the surface layer of the slab could not be scaled-off, cracks and irregularities on the steel sheet surface increased, and a smooth steel sheet surface could not be obtained. The surface characteristics were also determined to be poor when the amount of oxides (scales) generated suddenly increased, the interface between the steel substrate and oxides was roughened, and the surface quality after pickling and cold rolling degraded, or when some hot-rolling scales remained after pickling.


Structure observation was performed following the above-described procedure.


The evaluation results are shown in Tables 3 and 4.













TABLE 3










Steel structure






















Mean
Mean






Area
Area
Volume
grain
free



















Sheet
ratio of
ratio
fraction
size
path





Steel
thickness
F + BF
of TM
of RA
of RA
of BF
Balance



No.
ID
(mm)
(%)
(%)
(%)
(μm)
(μm)
structure
Remarks



















 1
A
2.3
69.1
 9.2
11.9
0.6
1.8
M + P + θ
Example


 2
B
2.0
68.4
 9.8
10.2
0.7
1.7
M + P + θ
Example


 3
C
2.3
67.8
11.1
12.2
0.7
2.0
M + P + θ
Example


 4
C
2.9
63.6
10.4
17.1
1.4
2.1
M + P + θ
Comparative











example


 5
C
2.5
62.2
11.1
16.8
1.3
2.4
M + P + θ
Comparative











example


 6
C
2.5
59.2
 9.7
6.8
0.6

5.6

M + P + θ
Comparative











example


 7
C
2.3
65.7
10.6
12.5

2.9

2.2
M + P + θ
Comparative











example


 8
C
1.9
64.9
12.2
15.4
1.4
2.4
M + P + θ
Comparative











example


 9
C
1.4
70.6
 8.9
3.8
0.5
2.5
M + P + θ
Comparative











example


10
C
1.4
66.9
 8.6
 9.1

3.8


5.2

M + P + θ
Comparative











example


11
C
2.0
64.2
1.2
5.7

3.0

2.6
M + P + θ
Comparative











example


12
C
2.1
66.4

23.4

 9.1

3.1

2.7
M + P + θ
Comparative











example


13
C
1.8
67.6
 5.6
6.7

3.4

2.4
M + P + θ
Comparative











example


14
C
1.7

85.6

 7.9
3.2
1.6
2.1
M + P + θ
Comparative











example


15
C
2.1
54.8

26.0

11.0
1.7
2.2
M + P + θ
Comparative











example


16
C
1.7
63.1

31.4

3.3

3.4

2.2
M + P + θ
Comparative











example


17
C
2.3
64.6
0.6
2.9
0.5
2.3
M + P + θ
Comparative











example


18
C
1.8
46.9

37.8

2.4
0.6
1.8
M + P + θ
Comparative











example


19
C
2.1
48.2
10.6
4.2
0.7
2.2
M + P + θ
Comparative











example


20
C
2.3
63.7
3.1
3.5
0.6
2.4
M + P + θ
Comparative











example


21
C
1.9
66.6
 9.6
14.4
0.8
2.5
M + P + θ
Example


22
D
1.6
59.9
12.1
14.5
1.1
1.9
M + P + θ
Example


23
E
1.6
66.6
11.6
11.4
1.2
1.8
M + P + θ
Example


24
F
1.9
67.4
10.8
10.9
0.9
1.7
M + P + θ
Example


25
G
1.5
68.4
 9.2
11.4
0.7
1.9
M + P + θ
Example


26
H
1.8
66.5
 8.4
12.8
0.9
1.5
M + P + θ
Example


27
I
2.1
58.2
12.8
15.6
0.8
2.0
M + P + θ
Example


28

J

2.3

83.3

 5.5
2.1
0.3
2.3
M + P + θ
Comparative











example


29

K

2.5
48.4

26.2

3.5
0.6
2.1
M + P + θ
Comparative











example


30

L

2.2

81.7

0.5
4.6
0.7
2.4
M + P + θ
Comparative











example


31
M
2.5
65.4
11.4
11.1
0.7
1.7
M + P + θ
Example


32
N
1.8
66.5
10.9
11.9
0.9
1.5
M + P + θ
Example


33
O
1.7
64.4
 9.7
12.8
1.1
1.2
M + P + θ
Example


34
P
1.7
67.7
 9.9
11.4
0.9
1.6
M + P + θ
Example


35
Q
2.4
64.5
10.6
11.4
1.0
1.1
M + P + θ
Example


36
R
1.8
68.2
11.2
 9.1
0.7
1.8
M + P + θ
Example


37
S
2.7
71.7
 8.9
 9.6
0.6
2.0
M + P + θ
Example


38
T
2.5
69.7
 9.7
10.1
0.5
1.2
M + P + θ
Example


39
U
1.8
67.6
10.4
11.4
0.7
1.5
M + P + θ
Example


40
V
2.5
65.4
10.1
12.5
0.5
1.8
M + P + θ
Example


41
W
2.3
63.0
11.8
13.6
0.6
1.1
M + P + θ
Example


42
X
1.9
68.4
 9.4
11.6
0.7
0.9
M + P + θ
Example


43
Y
2.5
66.1
10.6
12.8
0.9
1.5
M + P + θ
Example


44
Z
1.8
67.4
 9.7
12.5
0.9
1.6
M + P + θ
Example


45
AA
1.6
68.3
11.2
11.1
0.8
1.6
M + P + θ
Example


46
AB
2.0
66.9
12.4
13.2
0.9
1.7
M + P + θ
Example


47
AC
2.2
65.1
12.9
14.8
1.1
2.1
M + P + θ
Example


48
AD
1.8
66.2
10.8
12.1
0.7
1.9
M + P + θ
Example


49
AE
1.6
68.9
 9.2
10.9
0.6
1.6
M + P + θ
Example


50
AF
2.0
69.2
12.1
12.5
1.3
2.2
M + P + θ
Example


51
AG
1.8
68.9
11.6
11.4
1.4
2.3
M + P + θ
Example


52
AH
1.4
69.1
10.8
10.9
1.0
1.8
M + P + θ
Example


53
AI
1.8
67.5
12.2
11.4
0.9
2.2
M + P + θ
Example


54
AJ
1.3
66.6
11.4
13.8
0.7
2.4
M + P + θ
Example


55
AK
1.5
62.9
12.8
15.6
0.7
2.5
M + P + θ
Example


56
AL
2.0
61.9
11.9
22.5
0.9
1.9
M + P + θ
Example


57
AM
1.2
56.7
10.8
23.5
0.9
1.8
M + P + θ
Example


58
AN
1.4
64.1
 9.2
18.3
0.7
1.7
M + P + θ
Example


59
AO
1.4
61.3
11.6
21.3
0.8
1.9
M + P + θ
Example


60
AP
1.8
59.9
10.7
22.1
1.0
1.9
M + P + θ
Example


61
AQ
1.4
57.7
10.4
24.9
1.1
1.8
M + P + θ
Example





Underlined if outside of the appropriate range.


F: ferrite,


BF: bainitic ferrite,


RA: retained austenite,


M: martensite,


TM: tempered martensite,


P: peadite,


θ: cementite
























TABLE 4















Sheet
Sheet























Hole
Fatigue test results

passage
passage
























expansion
Fatigue


ability
ability
Surface


















Tensile test results
test results
limit


during
during
chamcteristics




















TS
EL
TS × EL
λ
strength
Fatigue

hot
cold
of final-



No.
(MPa)
(%)
(MPa · %)
(%)
(MPa)
ratio
Productivity
rolling
rolling
annealed sheet
Remarks





















 1
794
40.1
31839
68
450
0.57
High
High

Good
Example


 2
910
37.1
33761
52
460
0.51
High
High
High
Good
Example


 3
1008
33.5
33768
42
470
0.47
High
High

Good
Example


 4
1028
27.8
28578
35
410
0.40
Low
Low

Fairly poor
Comparative













example


 5
1034
27.2
28125
33
410
0.40
Low
Low

Fairly poor
Comparative













example


 6
1235
12.4
15314
26
500
0.40
Low
Low

Fairly poor
Comparative













example


 7
1012
18.9
19127
34
410
0.41
Low
High
Low
Poor
Comparative













example


 8
942
28.1
26470
42
400
0.42
Low
High

Good
Comparative













example


 9
679
34.1
23154
50
280
0.41
High
High

Good
Comparative













example


10
1044
15.8
16495
26
290
0.28
High
High
High
Good
Comparative













example


11
1189
16.2
19262
16
480
0.40
High
High
High
Good
Comparative













example


12
1022
18.4
18805
38
410
0.40
Low
High

Good
Comparative













example


13
1279
14.8
18929
24
520
0.41
High
High
High
Good
Comparative













example


14
682
26.9
18346
45
290
0.43
Low
High

Good
Comparative













example


15
1289
8.9
11472
24
510
0.40
High
High
High
Good
Comparative













example


16
802
20.5
16441
52
340
0.42
High
High

Good
Comparative













example


17
1030
27.6
28428
24
480
0.47
High
High

Good
Comparative













example


18
716
24.5
17542
53
300
0.42
High
High

Good
Comparative













example


19
1199
14.7
17625
21
480
0.40
High
High

Good
Comparative













example


20
1088
14.2
15450
14
490
0.45
High
High
High
Good
Comparative













example


21
1011
28.9
29218
35
430
0.43
Middle
High

Good
Example


22
1122
30.1
33772
36
470
0.42
High
High
High
Good
Example


23
1000
33.4
33400
38
430
0.43
High
High
High
Good
Example


24
1041
30.8
32063
35
440
0.42
High
High

Good
Example


25
984
34.5
33948
41
420
0.43
High
High
High
Good
Example


26
1008
33.1
33365
37
440
0.44
High
High

Good
Example


27
1211
27.8
33666
27
510
0.42
High
High
High
Good
Example


28
678
25.8
17492
68
310
0.46
High
High
High
Good
Comparative













example


29
1245
10.9
13571
14
520
0.42
High
High

Good
Comparative













example


30
679
26.9
18265
40
320
0.47
High
High
High
Good
Comparative













example


31
1056
30.1
31786
45
450
0.43
High
High

Good
Example


32
1047
29.8
31201
40
440
0.42
High
High
High
Good
Example


33
1070
28.4
30388
36
470
0.44
High
High

Good
Example


34
1004
32.9
33032
39
480
0.48
High
High
High
Good
Example


35
1007
32.4
32627
46
450
0.45
High
High

Good
Example


36
1004
33.9
34036
41
430
0.43
High
High
High
Good
Example


37
827
39.1
32336
51
410
0.50
High
High

Good
Example


38
908
35.5
32234
53
420
0.46
High
High

Good
Example


39
1001
33.6
33634
42
430
0.43
High
High
High
Good
Example


40
1033
32.0
33056
39
460
0.45
High
High

Good
Example


41
1107
28.9
31992
40
450
0.41
High
High
High
Good
Example


42
1002
33.7
33767
39
480
0.48
High
High

Good
Example


43
1039
32.6
33871
38
440
0.42
High
High

Good
Example


44
1026
32.8
33653
40
500
0.49
High
High
High
Good
Example


45
989
32.2
31846
56
450
0.46
High
High
High
Good
Example


46
1036
30.8
31909
62
460
0.44
High
High
High
Good
Example


47
1198
29.2
34982
48
510
0.43
High
High

Good
Example


48
996
32.1
31972
54
450
0.45
High
High
High
Good
Example


49
810
37.8
30618
61
440
0.54
High
High
High
Good
Example


50
822
34.1
28030
48
430
0.52
High
High

Good
Example


51
1014
27.9
28291
39
490
0.48
High
High

Good
Example


52
797
34.9
27815
45
400
0.50
High
High
High
Good
Example


53
1002
28.8
28858
38
470
0.47
High
High

Good
Example


54
1189
24.4
29012
31
520
0.44
High
High
High
Good
Example


55
1092
30.7
33524
37
490
0.45
High
High
High
Good
Example


56
1111
29.9
33219
33
520
0.47
High
High

Good
Example


57
1239
28.2
34940
28
560
0.45
High
High
High
Good
Example


58
985
30.6
30141
41
480
0.49
High
High
High
Good
Example


59
1134
28.7
32546
37
500
0.44
High
High
High
Good
Example


60
1122
28.2
31640
39
520
0.46
High
High

Good
Example


61
1086
31.9
34643
45
500
0.46
High
High
High
Good
Example









It can be seen that each of our examples has TS of 780 MPa or more, and the present disclosure enables manufacture of high-strength steel sheets with high productivity that are excellent not only in ductility but also in hole expansion formability (stretch flangeability) and fatigue properties. It can also be appreciated that each of our examples exhibits excellent sheet passage ability during hot rolling and cold rolling, as well as excellent surface characteristics of the final-annealed sheet.


In contrast, comparative examples are inferior in terms of one or more of tensile strength, ductility, balance between strength and ductility, hole expansion formability (stretch flangeability), fatigue properties, and productivity.

Claims
  • 1. A method for manufacturing a high-strength steel sheet, the method comprising: preparing a steel slab containing, in mass %, C: 0.10% or more and 0.35% or less, Si: 0.50% or more and 2.50% or less, Mn: 2.00% or more and less than 3.50%, P: 0.001% or more and 0.100% or less, S: 0.0001% or more and 0.0200% or less, and N: 0.0005% or more and 0.0100% or less, and the balance consisting of Fe and incidental impurities;subjecting the steel slab to hot rolling by heating the steel slab to a temperature of 1100° C. or higher and 1300° C. or lower, hot rolling the steel slab with a finisher delivery temperature of 800° C. or higher and 1000° C. or lower to form a hot-rolled steel sheet, and coiling the hot-rolled steel sheet at a mean coiling temperature of 200° C. or higher and 500° C. or lower;subjecting the hot-rolled steel sheet to pickling treatment;subjecting the hot-rolled steel sheet to annealing by retaining the hot-rolled steel sheet at a temperature of 740° C. or higher and 840° C. or lower for 10 s or more and 900 s or less, and then cooling the hot-rolled steel sheet at a mean cooling rate of 5° C./s or higher and 30° C./s or lower to a cooling stop temperature of 150° C. or higher and 350° C. or lower; andsubjecting the hot-rolled steel sheet to reheating treatment by reheating the hot-rolled steel sheet to a reheating temperature of higher than 350° C. and 550° C. or lower, and retaining the hot-rolled steel sheet at the reheating temperature for 10 s or more.
  • 2. The method for manufacturing a high-strength steel sheet according to claim 1, the method further comprising prior to the annealing, cold rolling the hot-rolled steel sheet at a rolling reduction of less than 30% to form a cold-rolled steel sheet, wherein in the annealing, the cold-rolled steel sheet is retained at a temperature of 740° C. or higher and 840° C. or lower for 10 s or more and 900 s or less, and cooled at a mean cooling rate of 5° C./s or higher and 30° C./s or lower to a cooling stop temperature of 150° C. or higher and 350° C. or lower, andin the reheating treatment, the cold-rolled steel sheet is reheated to a reheating temperature of higher than 350° C. and 550° C. or lower and retained at the reheating temperature for 10 s or more.
  • 3. The method for manufacturing a high-strength steel sheet according to claim 1, the method further comprising after the reheating treatment, subjecting the hot-rolled steel sheet or the cold-rolled steel sheet to galvanizing treatment.
  • 4. The method for manufacturing a high-strength steel sheet according to claim 1, wherein the steel slab further contains, in mass %, at least one element selected from the group consisting of Ti: 0.005% or more and 0.100% or less and B: 0.0001% or more and 0.0050% or less.
  • 5. The method for manufacturing a high-strength steel sheet according to claim 1, wherein the steel slab further contains, in mass %, at least one element selected from the group consisting of Al: 0.01% or more and 1.00% or less, Nb: 0.005% or more and 0.100% or less, Cr: 0.05% or more and 1.00% or less, Cu: 0.05% or more and 1.00% or less, Sb: 0.002% or more and 0.200% or less, Sn: 0.002% or more and 0.200% or less, Ta: 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, and REM: 0.0005% or more and 0.0050% or less.
  • 6. A high-strength steel sheet comprising: a steel chemical composition containing, in mass %, C: 0.10% or more and 0.35% or less, Si: 0.50% or more and 2.50% or less, Mn: 2.00% or more and less than 3.50%, P: 0.001% or more and 0.100% or less, S: 0.0001% or more and 0.0200% or less, and N: 0.0005% or more and 0.0100% or less, and the balance consisting of Fe and incidental impurities; anda steel structure that contains a total of 30% or more and 75% or less by area of ferrite and bainitic ferrite, 5% or more and 15% or less by area of tempered martensite, and 8% or more by volume of retained austenite,wherein the retained austenite has a mean grain size of 2 μm or less and the bainitic ferrite has a mean free path of 3 μm or less.
  • 7. The high-strength steel sheet according to claim 6, wherein the steel chemical composition further contains, in mass %, at least one element selected from the group consisting of Ti: 0.005% or more and 0.100% or less and B: 0.0001% or more and 0.0050% or less.
  • 8. The high-strength steel sheet according to claim 6, wherein the steel chemical composition further contains, in mass %, at least one element selected from the group consisting of Al: 0.01% or more and 1.00% or less, Nb: 0.005% or more and 0.100% or less, Cr: 0.05% or more and 1.00% or less, Cu: 0.05% or more and 1.00% or less, Sb: 0.002% or more and 0.200% or less, Sn: 0.002% or more and 0.200% or less, Ta: 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, and REM: 0.0005% or more and 0.0050% or less.
  • 9. The method for manufacturing a high-strength steel sheet according to claim 2, the method further comprising after the reheating treatment, subjecting the hot-rolled steel sheet or the cold-rolled steel sheet to galvanizing treatment.
  • 10. The method for manufacturing a high-strength steel sheet according to claim 2, wherein the steel slab further contains, in mass %, at least one element selected from the group consisting of Ti: 0.005% or more and 0.100% or less and B: 0.0001% or more and 0.0050% or less.
  • 11. The method for manufacturing a high-strength steel sheet according to claim 3, wherein the steel slab further contains, in mass %, at least one element selected from the group consisting of Ti: 0.005% or more and 0.100% or less and B: 0.0001% or more and 0.0050% or less.
  • 12. The method for manufacturing a high-strength steel sheet according to claim 9, wherein the steel slab further contains, in mass %, at least one element selected from the group consisting of Ti: 0.005% or more and 0.100% or less and B: 0.0001% or more and 0.0050% or less.
  • 13. The method for manufacturing a high-strength steel sheet according to claim 2, wherein the steel slab further contains, in mass %, at least one element selected from the group consisting of Al: 0.01% or more and 1.00% or less, Nb: 0.005% or more and 0.100% or less, Cr: 0.05% or more and 1.00% or less, Cu: 0.05% or more and 1.00% or less, Sb: 0.002% or more and 0.200% or less, Sn: 0.002% or more and 0.200% or less, Ta: 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, and REM: 0.0005% or more and 0.0050% or less.
  • 14. The method for manufacturing a high-strength steel sheet according to claim 3, wherein the steel slab further contains, in mass %, at least one element selected from the group consisting of Al: 0.01% or more and 1.00% or less, Nb: 0.005% or more and 0.100% or less, Cr: 0.05% or more and 1.00% or less, Cu: 0.05% or more and 1.00% or less, Sb: 0.002% or more and 0.200% or less, Sn: 0.002% or more and 0.200% or less, Ta: 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, and REM: 0.0005% or more and 0.0050% or less.
  • 15. The method for manufacturing a high-strength steel sheet according to claim 4, wherein the steel slab further contains, in mass %, at least one element selected from the group consisting of Al: 0.01% or more and 1.00% or less, Nb: 0.005% or more and 0.100% or less, Cr: 0.05% or more and 1.00% or less, Cu: 0.05% or more and 1.00% or less, Sb: 0.002% or more and 0.200% or less, Sn: 0.002% or more and 0.200% or less, Ta: 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, and REM: 0.0005% or more and 0.0050% or less.
  • 16. The method for manufacturing a high-strength steel sheet according to claim 9, wherein the steel slab further contains, in mass %, at least one element selected from the group consisting of Al: 0.01% or more and 1.00% or less, Nb: 0.005% or more and 0.100% or less, Cr: 0.05% or more and 1.00% or less, Cu: 0.05% or more and 1.00% or less, Sb: 0.002% or more and 0.200% or less, Sn: 0.002% or more and 0.200% or less, Ta: 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, and REM: 0.0005% or more and 0.0050% or less.
  • 17. The method for manufacturing a high-strength steel sheet according to claim 10, wherein the steel slab further contains, in mass %, at least one element selected from the group consisting of Al: 0.01% or more and 1.00% or less, Nb: 0.005% or more and 0.100% or less, Cr: 0.05% or more and 1.00% or less, Cu: 0.05% or more and 1.00% or less, Sb: 0.002% or more and 0.200% or less, Sn: 0.002% or more and 0.200% or less, Ta: 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, and REM: 0.0005% or more and 0.0050% or less.
  • 18. The method for manufacturing a high-strength steel sheet according to claim 11, wherein the steel slab further contains, in mass %, at least one element selected from the group consisting of Al: 0.01% or more and 1.00% or less, Nb: 0.005% or more and 0.100% or less, Cr: 0.05% or more and 1.00% or less, Cu: 0.05% or more and 1.00% or less, Sb: 0.002% or more and 0.200% or less, Sn: 0.002% or more and 0.200% or less, Ta: 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, and REM: 0.0005% or more and 0.0050% or less.
  • 19. The method for manufacturing a high-strength steel sheet according to claim 12, wherein the steel slab further contains, in mass %, at least one element selected from the group consisting of Al: 0.01% or more and 1.00% or less, Nb: 0.005% or more and 0.100% or less, Cr: 0.05% or more and 1.00% or less, Cu: 0.05% or more and 1.00% or less, Sb: 0.002% or more and 0.200% or less, Sn: 0.002% or more and 0.200% or less, Ta: 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, and REM: 0.0005% or more and 0.0050% or less.
  • 20. The high-strength steel sheet according to claim 7, wherein the steel chemical composition further contains, in mass %, at least one element selected from the group consisting of Al: 0.01% or more and 1.00% or less, Nb: 0.005% or more and 0.100% or less, Cr: 0.05% or more and 1.00% or less, Cu: 0.05% or more and 1.00% or less, Sb: 0.002% or more and 0.200% or less, Sn: 0.002% or more and 0.200% or less, Ta: 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, and REM: 0.0005% or more and 0.0050% or less.
Priority Claims (1)
Number Date Country Kind
2014-161677 Aug 2014 JP national
PCT Information
Filing Document Filing Date Country Kind
PCT/JP2015/003947 8/5/2015 WO 00