HIGH STRENGTH STEEL SHEET AND METHOD FOR MANUFACTURING THE SAME

Abstract
A high strength steel sheet includes a specific microstructure having a specific chemical composition and satisfying the formulas (1) and (2) defined below:
Description
FIELD OF THE INVENTION

The present invention relates to a high strength steel sheet excellent in tensile strength and delayed fracture resistance, and to a method for manufacturing the same. The high strength steel sheet according to aspects of the present invention may be suitably used as structural members, such as automobile parts.


BACKGROUND OF THE INVENTION

Steel sheets for automobiles are being increased in strength to reduce CO2 emissions by weight reduction of vehicles and to enhance crashworthiness by weight reduction of automobile bodies at the same time, with introduction of new laws and regulations one after another. To increase the strength of automobile bodies, high strength steel sheets having a tensile strength (TS) of 1320 MPa or higher class are increasingly applied to principal structural parts of automobiles.


High strength steel sheets used for automobiles are required to have an excellent yield ratio (YR=yield strength YS/tensile strength TS) from the point of view of performance of parts. For example, automobile frame parts, such as bumpers, are required to exhibit excellent impact absorption at the time of collision. Thus, steel sheets that have excellent YR correlated with impact absorption are favorably used.


Automobile frame parts have many end faces formed by shearing. The morphology of a sheared end face depends on the shear clearance. The morphology of a sheared end face affects delayed fracture resistance. Here, delayed fracture is a phenomenon in which, when a formed part is placed in a hydrogen penetration environment, hydrogen penetrates into the steel sheet constituting the part to cause a decrease in interatomic bonding force or to cause local deformation, thus giving rise to microcracks that grow to fracture. High strength steel sheets used for automobiles are required to have a wide range of appropriate clearances not leading to delayed fracture.


To cope with these demands, for example, Patent Literature 1 provides a high strength steel sheet having a tensile strength of 980 MPa or more and excellent bending formability, and a method for manufacturing the same. However, the technique described in Patent Literature 1 does not consider YR or the range of appropriate clearances not leading to delayed fracture. Furthermore, the steel sheets described in Patent Literature 1 do not achieve YR≥85%.


For example, Patent Literature 2 provides a high strength steel sheet having a tensile strength of 1320 MPa or more and excellent delayed fracture resistance at sheared end faces, and a method for manufacturing the same. However, the technique described in Patent Literature 2 does not consider the range of appropriate clearances not leading to delayed fracture.


For example, Patent Literature 3 provides a high strength steel sheet having a tensile strength of 1100 MPa or more and being excellent in YR, surface quality, and weldability, and a method for manufacturing the same. However, the technique described in Patent Literature 3 does not consider the range of appropriate clearances not leading to delayed fracture.


PATENT LITERATURE





    • PTL 1: Japanese Patent No. 6354909

    • PTL 2: Japanese Patent No. 6112261

    • PTL 3: Japanese Patent No. 6525114





SUMMARY OF THE INVENTION

Aspects of the present invention have been developed in view of the circumstances discussed above. Objects according to aspects of the present invention are therefore to provide a high strength steel sheet having a TS of 1320 MPa or more and a YR of 85% or more and having a wide range of appropriate clearances not leading to delayed fracture; and to provide a method for manufacturing the same.


The present inventors carried out extensive studies directed to solving the problems described above and have consequently found the following facts.

    • (1) 1320 MPa or higher TS can be achieved by limiting tempered martensite to 85% or more.
    • (2) 85% or higher YR can be achieved by limiting retained austenite to less than 58, KAM (S)/KAM (C) to less than 1.00, and further Hv (Q)-Hv (S) to 8 or more.
    • (3) A wide range of appropriate clearances not leading to delayed fracture can be achieved by limiting KAM (S)/KAM (C) to less than 1.00 and further Hv (Q)-Hv (S) to 8 or more.


Aspects of the present invention have been made based on the above findings. Specifically, a summary of configurations according to aspects of the present invention is as follows.


[1] A high strength steel sheet including a microstructure having a chemical composition including, by mass:

    • C: 0.15% or more and 0.45% or less,
    • Si: 0.10% or more and 2.00% or less,
    • Mn: 0.5% or more and 3.5% or less,
    • P: 0.100% or less,
    • S: 0.0200% or less,
    • Al: 0.010% or more and 1.000% or less,
    • N: 0.0100% or less, and
    • H: 0.0020% or less,
    • the balance being Fe and incidental impurities;
    • the microstructure being such that:
    • the area fraction of tempered martensite is 85% or more,
    • the volume fraction of retained austenite is less than 5%, and
    • the area fraction of the total of ferrite and bainitic ferrite is 10% or less;
    • the microstructure satisfying the formulas (1) and (2) defined below:











KAM

(
S
)

/

KAM

(
C
)


<
1.




(
1
)









    • wherein KAM (S) is a KAM (Kernel average misorientation) value of a superficial portion of the steel sheet, and KAM (C) is a KAM value of a central portion of the steel sheet,














Hv

(
Q
)

-

Hv

(
S
)



8




(
2
)









    • wherein Hv (Q) indicates the hardness of a portion at ¼ sheet thickness and Hv (S) indicates the hardness of a superficial portion of the steel sheet.


      [2] The high strength steel sheet described in [1], wherein the chemical composition further includes one, or two or more elements selected from, by mass %:

    • Ti: 0.100% or less,

    • B: 0.0100% or less,

    • Nb: 0.100% or less,

    • Cu: 1.00% or less,

    • Cr: 1.00% or less,

    • V: 0.100% or less,

    • Mo: 0.500% or less,

    • Ni: 0.50% or less,

    • Sb: 0.200% or less,

    • Sn: 0.200% or less,

    • As: 0.100% or less,

    • Ta: 0.100% or less,

    • Ca: 0.0200% or less,

    • Mg: 0.0200% or less,

    • Zn: 0.020% or less,

    • Co: 0.020% or less,

    • Zr: 0.020% or less, and

    • REM: 0.0200% or less.


      [3] The high strength steel sheet described in [1] or [2], which has a coated layer on a surface of the steel sheet.


      [4] A method for manufacturing a high strength steel sheet described in [1] or [2], the method including:

    • providing a cold rolled steel sheet produced by subjecting a steel slab to hot rolling, pickling, and cold rolling;

    • annealing the steel sheet under conditions where:

    • a temperature T1 is 850° C. or above and 1000° C. or below and a holding time t1 at T1 is 10 seconds or more and 1000 seconds or less;

    • cooling the steel sheet to 100° C. or below;

    • starting working at an elapsed time t2 of 1000 seconds or less from the time when the temperature reaches 100° C.,

    • the working being performed under conditions where:

    • a working start temperature T2 is 80° C. or below and an equivalent plastic strain is 0.10% or more and 5.00% or less;

    • tempering the steel sheet under conditions where:

    • a temperature T3 is 100° C. or above and 400° C. or below and a holding time t3 at T3 is 1.0 second or more and 1000.0 seconds or less; and

    • cooling the steel sheet under conditions where a cooling rate θ1 from T3 to 80° C. is 100° C./sec or less.


      [5] The method for manufacturing a high strength steel sheet described in [4], wherein the working before the tempering is performed under conditions where strain is applied by two or more separate working operations, and the total of the equivalent plastic strains applied in the working operations is 0.10% or more.


      [6] The method for manufacturing a high strength steel sheet described in [4] or [5], further including performing coating treatment during the annealing or after the annealing.





According to aspects of the present invention, a high strength steel sheet can be obtained that has a TS of 1320 MPa or more and a YR of 85% or more and has a wide range of appropriate clearances not leading to delayed fracture. Furthermore, for example, the high strength steel sheet according to aspects of the present invention may be applied to automobile structural members to reduce the weight of automobile bodies and thereby to enhance fuel efficiency. Thus, aspects of the present invention are highly valuable in industry.







DETAILED DESCRIPTION OF EMBODIMENTS OF THE INVENTION

Embodiments of the present invention will be described below.


First, appropriate ranges of the chemical composition of the high strength steel sheet and the reasons why the chemical composition is thus limited will be described. In the following description, “%” indicating the contents of constituent elements of steel means “mass %” unless otherwise specified.


C: 0.15% or More and 0.45% or Less

Carbon is one of the important basic components of steel, and, particularly in accordance with aspects of the present invention, is an important element that affects TS. If the C content is less than 0.15%, it is difficult to achieve 1320 MPa or higher TS. Thus, the C content is limited to 0.15% or more. The C content is preferably 0.16% or more. The C content is more preferably 0.17% or more. The C content is still more preferably 0.18% or more. The C content is most preferably 0.19% or more. However, if the C content is more than 0.45%, the ultimate deformability of the steel is lowered and the range of appropriate clearances not leading to delayed fracture is narrowed. Thus, the C content is limited to 0.45% or less. The C content is preferably 0.40% or less. The C content is more preferably 0.35% or less. The C content is still more preferably 0.30% or less. The C content is most preferably 0.26% or less.


Si: 0.10% or More and 2.00% or Less

Silicon is one of the important basic components of steel, and, particularly in accordance with aspects of the present invention, is an important element that affects TS and retained austenite. If the Si content is less than 0.10%, 1320 MPa or higher TS is hardly achieved. Thus, the Si content is limited to 0.10% or more. The Si content is preferably 0.15% or more. The Si content is more preferably 0.20% or more. The Si content is still more preferably 0.30% or more. The Si content is most preferably 0.40% or more. However, if the Si content is more than 2.00%, the amount of retained austenite excessively increases to make it difficult to achieve 85% or higher YR. Thus, the Si content is limited to 2.00% or less. The Si content is preferably 1.80% or less. The Si content is more preferably 1.60% or less. The Si content is still more preferably 1.50% or less. The Si content is most preferably 1.20% or less.


Mn: 0.5% or More and 3.5% or Less

Manganese is one of the important basic components of steel, and, particularly in accordance with aspects of the present invention, is an important element that affects the fraction of ferrite and the fraction of bainite. If the Mn content is less than 0.5%, the fraction of ferrite and the fraction of bainite are increased to make it difficult to achieve 1320 MPa or higher TS and to achieve 85% or higher YR. Thus, the Mn content is limited to 0.5% or more. The Mn content is preferably 0.7% or more. The Mn content is more preferably 1.08 or more. The Mn content is still more preferably 1.1% or more. The Mn content is most preferably 1.5% or more. However, if the Mn content is more than 3.5%, manganese macro-segregation occurs to lower the ultimate deformability of the steel and thereby to narrow the range of appropriate clearances not leading to delayed fracture. Thus, the Mn content is limited to 3.5% or less. The Mn content is preferably 3.3% or less. The Mn content is more preferably 3.1% or less. The Mn content is still more preferably 3.0% or less. The Mn content is most preferably 2.8% or less.


P: 0.100% or Less

If the P content is more than 0.100%, phosphorus is segregated at grain boundaries to make the steel sheet brittle and to narrow the range of appropriate clearances not leading to delayed fracture. Thus, the P content is limited to 0.100% or less. The P content is preferably 0.080% or less. The P content is more preferably 0.060% or less. The lower limit of the P content is not particularly limited but is preferably 0.001% or more due to production technology limitations.


S: 0.0200% or Less

If the S content is more than 0.0200%, sulfides are formed making the ultimate deformability of the steel lower and thereby narrow the range of appropriate clearances not leading to delayed fracture. Thus, the S content is limited to 0.0200% or less. The S content is preferably 0.0100% or less. The S content is more preferably 0.0050% or less. The lower limit of the S content is not particularly limited but is preferably 0.0001% or more due to production technology limitations.


Al: 0.010% or More and 1.000% or Less

The addition of aluminum increases the strength of the steel sheet and facilitates achieving 1320 MPa or higher TS. To obtain these effects, the Al content needs to be 0.010% or more. Thus, the Al content is limited to 0.010% or more. The Al content is preferably 0.012% or more. The Al content is more preferably 0.015% or more. The Al content is still more preferably 0.020% or more. However, if the Al content is more than 1.000%, the fraction of ferrite and the fraction of bainite increase to make it difficult to achieve 1320 MPa or higher TS and to achieve 85% or higher YR. Thus, the Al content is limited to 1.000% or less. The Al content is preferably 0.500% or less. The Al content is more preferably 0.100% or less.


N: 0.0100% or Less

If the N content is more than 0.0100%, the cast slab becomes brittle and is easily cracked to cause a significant decrease in productivity. Thus, the N content is limited to 0.0100% or less. The N content is preferably 0.0080% or less. The N content is more preferably 0.0070% or less. The N content is still more preferably 0.0060% or less. The N content is most preferably 0.0050% or less. The lower limit of the N content is not particularly limited but is preferably 0.0010% or more due to production technology limitations.


H: 0.0020% or Less

If the H content exceeds not more than 0.0020%, the ultimate deformability of the steel is lowered and the range of appropriate clearances not leading to delayed fracture is narrowed. Thus, the H content is limited to 0.0020% or less. The H content is preferably 0.0015% or less. The H content is more preferably 0.0010% or less. The lower limit of the H content is not particularly limited. The H content may be 0% because the lower the H content, the wider the range of appropriate clearances not leading to delayed fracture.


In addition to the chemical composition described above, the high strength steel sheet according to aspects of the present invention preferably further contains one, or two or more elements selected from, by mass %, Ti: 0.100% or less, B: 0.0100% or less, Nb: 0.100% or less, Cu: 1.00% or less, Cr: 1.00% or less, V: 0.100% or less, Mo: 0.500% or less, Ni: 0.50% or less, Sb: 0.200% or less, Sn: 0.200% or less, As: 0.100% or less, Ta: 0.100% or less, Ca: 0.0200% or less, Mg: 0.0200% or less, Zn: 0.020% or less, Co: 0.020% or less, Zr: 0.020% or less, and REM: 0.0200% or less.


Ti: 0.100% or Less

If the Ti content is more than 0.100%, the cast slab becomes brittle and is easily cracked to cause a significant decrease in productivity. Thus, when titanium is added, the content thereof is limited to 0.100% or less. The Ti content is preferably 0.075% or less. The Ti content is more preferably 0.050% or less. The Ti content is still more preferably less than 0.050%. In contrast, the addition of titanium increases the strength of the steel sheet and facilitates achieving 1320 MPa or higher TS. To obtain these effects, the Ti content is preferably 0.001% or more. The Ti content is more preferably 0.005% or more. The Ti content is still more preferably 0.010% or more.


B: 0.0100% or Less

If the B content is more than 0.0100%, the cast slab becomes brittle and is easily cracked to cause a significant decrease in productivity. Thus, when boron is added, the content thereof is limited to 0.0100% or less. The B content is preferably 0.0080% or less. The B content is more preferably 0.0050% or less. In contrast, the addition of boron increases the strength of the steel sheet and facilitates achieving 1320 MPa or higher TS. To obtain these effects, the B content is preferably 0.0001% or more. The B content is more preferably 0.0002% or more.


Nb: 0.100% or Less

If the Nb content is more than 0.100%, the cast slab becomes brittle and is easily cracked to cause a significant decrease in productivity. Thus, when niobium is added, the content thereof is limited to 0.100% or less. The Nb content is preferably 0.090% or less. The Nb content is more preferably 0.050% or less. The Nb content is still more preferably 0.030% or less. In contrast, the addition of niobium increases the strength of the steel sheet and facilitates achieving 1320 MPa or higher TS. To obtain these effects, the Nb content is preferably 0.001% or more. The Nb content is more preferably 0.002% or more.


Cu: 1.00% or Less

If the Cu content is more than 1.00%, the cast slab becomes brittle and is easily cracked to cause a significant decrease in productivity. Thus, when copper is added, the Cu content is limited to 1.00% or less. The Cu content is preferably 0.50% or less. In contrast, copper suppresses the penetration of hydrogen into the steel sheet and improves the range of appropriate clearances not leading to delayed fracture. To obtain these effects, the Cu content is preferably 0.01% or more. The Cu content is preferably 0.03% or more. The Cu content is more preferably 0.10% or more.


Cr: 1.00% or Less

If the Cr content is more than 1.00%, large amounts of coarse precipitates and inclusions are formed to lower the ultimate deformability of the steel, thus narrowing the range of appropriate clearances for hole expanding deformation. Thus, when chromium is added, the content thereof is limited to 1.00% or less. The Cr content is preferably 0.70% or less. The Cr content is more preferably 0.50% or less. In contrast, chromium not only serves as a solid solution strengthening element but also can stabilize austenite and suppress ferrite formation in the cooling process during continuous annealing, thus increasing the strength of the steel sheet. To obtain these effects, the Cr content is preferably 0.01% or more. The Cr content is more preferably 0.02% or more.


V: 0.100% or Less

If the V content is more than 0.100%, large amounts of coarse precipitates and inclusions are formed to lower the ultimate deformability of the steel, thus narrowing the range of appropriate clearances for hole expanding deformation. Thus, when vanadium is added, the content thereof is limited to 0.100% or less. The V content is preferably 0.060% or less. In contrast, vanadium increases the strength of the steel sheet. To obtain this effect, the V content is preferably 0.001% or more. The V content is more preferably 0.005% or more. The V content is still more preferably 0.010% or more.


Mo: 0.500% or Less

If the Mo content is more than 0.500%, large amounts of coarse precipitates and inclusions are formed to lower the ultimate deformability of the steel, thus narrowing the range of appropriate clearances for hole expanding deformation. Thus, when molybdenum is added, the content thereof is limited to 0.500% or less. The Mo content is preferably 0.450% or less. The Mo content is more preferably 0.400% or less. In contrast, molybdenum not only serves as a solid solution strengthening element but also can stabilize austenite and suppress ferrite formation in the cooling process during continuous annealing, thus increasing the strength of the steel sheet. To obtain these effects, the Mo content is preferably 0.010% or more. The Mo content is more preferably 0.020% or more.


Ni: 0.50% or Less

If the Ni content is more than 0.50%, large amounts of coarse precipitates and inclusions are formed to lower the ultimate deformability of the steel, thus narrowing the range of appropriate clearances for hole expanding deformation. Thus, when nickel is added, the content thereof is limited to 0.50% or less. The Ni content is preferably 0.45% or less. The Ni content is more preferably 0.30% or less. In contrast, nickel can stabilize austenite and suppress ferrite formation in the cooling process during continuous annealing, thus increasing the strength of the steel sheet. To obtain these effects, the Ni content is preferably 0.01% or more. The Ni content is more preferably 0.02% or more.


Sb: 0.200% or Less

If the Sb content is more than 0.200%, large amounts of coarse precipitates and inclusions are formed to lower the ultimate deformability of the steel, thus narrowing the range of appropriate clearances for hole expanding deformation. Thus, when antimony is added, the content thereof is limited to 0.200% or less. The Sb content is preferably 0.100% or less. The Sb content is more preferably 0.050% or less. In contrast, antimony suppresses the formation of a soft superficial layer and increases the strength of the steel sheet. To obtain these effects, the Sb content is preferably 0.001% or more. The Sb content is more preferably 0.005% or more.


Sn: 0.200% or Less

If the Sn content is more than 0.200%, large amounts of coarse precipitates and inclusions are formed to lower the ultimate deformability of the steel, thus narrowing the range of appropriate clearances for hole expanding deformation. Thus, when tin is added, the content thereof is limited to 0.200% or less. The Sn content is preferably 0.100% or less. The Sn content is more preferably 0.050% or less. In contrast, tin suppresses the formation of a soft superficial layer and increases the strength of the steel sheet. To obtain these effects, the Sn content is preferably 0.001% or more. The Sn content is more preferably 0.005% or more.


As: 0.100% or Less

If the As content is more than 0.100%, large amounts of coarse precipitates and inclusions are formed to lower the ultimate deformability of the steel, thus narrowing the range of appropriate clearances for hole expanding deformation. Thus, when arsenic is added, the content thereof is limited to 0.100% or less. The As content is preferably 0.060% or less. The As content is more preferably 0.010% or less. Arsenic increases the strength of the steel sheet. To obtain this effect, the As content is preferably 0.001% or more. The As content is more preferably 0.005% or more.


Ta: 0.100% or Less

If the Ta content is more than 0.100%, large amounts of coarse precipitates and inclusions are formed to lower the ultimate deformability of the steel, thus narrowing the range of appropriate clearances for hole expanding deformation. Thus, when tantalum is added, the content thereof is limited to 0.100% or less. The Ta content is preferably 0.050% or less. The Ta content is more preferably 0.010% or less. On the other hand, tantalum increases the strength of the steel sheet. To obtain this effect, the Ta content is preferably 0.001% or more. The Ta content is more preferably 0.005% or more.


Ca: 0.0200% or Less

If the Ca content is more than 0.0200%, large amounts of coarse precipitates and inclusions are formed to lower the ultimate deformability of the steel, thus narrowing the range of appropriate clearances for hole expanding deformation. Thus, when calcium is added, the content thereof is limited to 0.0200% or less. The Ca content is preferably 0.0100% or less. In contrast, calcium is an element used for deoxidation, and furthermore this element is effective for controlling the shape of sulfides to spherical, enhancing the ultimate deformability of the steel sheet, and enhancing the range of appropriate clearances not leading to delayed fracture. To obtain these effects, the Ca content is preferably 0.0001% or more.


Mg: 0.0200% or Less

If the Mg content is more than 0.0200%, large amounts of coarse precipitates and inclusions are formed to lower the ultimate deformability of the steel, thus narrowing the range of appropriate clearances for hole expanding deformation. Thus, when magnesium is added, the content thereof is limited to 0.0200% or less. In contrast, magnesium is an element used for deoxidation, and furthermore this element is effective for controlling the shape of sulfides to spherical, enhancing the ultimate deformability of the steel sheet, and enhancing the range of appropriate clearances not leading to delayed fracture. To obtain these effects, the Mg content is preferably 0.0001% or more.


Zn: 0.020% or Less, Co: 0.020% or Less, Zr: 0.020% or Less

If the contents of zinc, cobalt, and zirconium are each more than 0.020%, large amounts of coarse precipitates and inclusions are formed to lower the ultimate deformability of the steel, thus narrowing the range of appropriate clearances for hole expanding deformation. Thus, when zinc, cobalt, and zirconium are added, the contents thereof are each limited to 0.020% or less. In contrast, zinc, cobalt, and zirconium are elements effective for controlling the shape of inclusions to spherical, enhancing the ultimate deformability of the steel sheet, and enhancing the range of appropriate clearances not leading to delayed fracture. To obtain these effects, the contents of zinc, cobalt, and zirconium are preferably each 0.0001% or more.


REM: 0.0200% or Less

If the REM content is more than 0.0200%, large amounts of coarse precipitates and inclusions are formed to lower the ultimate deformability of the steel, thus narrowing the range of appropriate clearances for hole expanding deformation. Thus, when rare earth metals are added, the content thereof is limited to 0.0200% or less. In contrast, rare earth metals are elements effective for controlling the shape of inclusions to spherical, enhancing the ultimate deformability of the steel sheet, and enhancing the range of appropriate clearances not leading to delayed fracture. To obtain these effects, the REM content is preferably 0.0001% or more.


The balance of the composition is Fe and incidental impurities. When the content of any of the above optional elements is below the lower limit, the element does not impair the advantageous effects according to aspects of the present invention. Thus, such an optional element below the lower limit content is regarded as an incidental impurity.


Next, the steel microstructure of the high strength steel sheet according to aspects of the present invention will be described.


Tempered Martensite: 85% or More in Terms of Area Fraction

This requirement is a highly important claim component in accordance with aspects of the present invention. 1320 MPa or higher TS may be achieved by making martensite as the main phase. To obtain this effect, the area fraction of tempered martensite needs to be 85% or more. Thus, the area fraction of tempered martensite is limited to 85% or more. The area fraction of tempered martensite is preferably 90% or more. The area fraction of tempered martensite is more preferably 92% or more and is further preferably 95% or more. On the other hand, the upper limit of the area fraction of tempered martensite is not particularly limited and may be 100%.


Here, tempered martensite is measured as follows. A longitudinal cross section of the steel sheet is polished and is subjected to etching in 3 vol % Nital solution. A portion at ¼ sheet thickness (a location corresponding to ¼ of the sheet thickness in the depth direction from the steel sheet surface) is observed using SEM in 10 fields of view at a magnification of ×2000. In the microstructure images, tempered martensite is structures that have fine irregularities inside the structures and contain carbides within the structures. The values thus obtained are averaged to determine the area fraction of tempered martensite.


Retained Austenite: Less than 5% in Terms of Volume Fraction


This requirement is a highly important claim component in accordance with aspects of the present invention. If the volume fraction of retained austenite is 5% or more, it is difficult to achieve 85% or higher YR. The lowering in YR is ascribed to the fact that the amount of retained austenite is so large that strain induced transformation of retained austenite results in low YS. Thus, retained austenite is limited to less than 5% and is preferably 4% or less. The lower limit of retained austenite is not particularly limited. A lower fraction of retained austenite is more preferable, and the fraction may be 0%.


Here, retained austenite is measured as follows. The steel sheet was polished to expose a face 0.1 mm below ¼ sheet thickness and was thereafter further chemically polished to expose a face 0.1 mm below the face exposed above. The face was analyzed with an X-ray diffractometer using CoKα radiation to determine the integral intensity ratios of the diffraction peaks of {200}, {220}, and {311} planes of fcc iron and {200}, {211}, and {220} planes of bcc iron. Nine integral intensity ratios thus obtained were averaged to determine retained austenite.


Total of Ferrite and Bainitic Ferrite: 10% or Less in Terms of Area Fraction

This requirement is a highly important claim component in accordance with aspects of the present invention. If the total of ferrite and bainitic ferrite is more than 10%, it is difficult to achieve 1320 MPa or higher TS and to achieve 85% or higher YR. The lowering in YR is ascribed to the fact that ferrite and bainitic ferrite are soft microstructures and hasten the occurrence of yielding. Thus, the total of ferrite and bainitic ferrite is limited to 10% or less. The total is preferably 8% or less and is more preferably 5% or less. The lower limit of the total of ferrite and bainitic ferrite is not particularly limited. A smaller fraction is more preferable. The lower limit of the total of ferrite and bainitic ferrite may be 0%.


Here, the total of ferrite and bainitic ferrite is measured as follows. A longitudinal cross section of the steel sheet is polished and is subjected to etching in 3 vol % Nital solution. A portion at ¼ sheet thickness (a location corresponding to ¼ of the sheet thickness in the depth direction from the steel sheet surface) is observed using SEM in 10 fields of view at a magnification of ×2000. In the microstructure images, ferrite and bainitic ferrite are recessed structures with a flat interior. The values thus obtained are averaged to determine the total of ferrite and bainitic ferrite.


Possible microstructures other than those described above include pearlite, fresh martensite, and acicular ferrite. These microstructures do not affect characteristics as long as their fractions do not exceed 58, and thus may be present within that range.

    • KAM (S)/KAM (C)<1.00


KAM (S): KAM (Kernel Average Misorientation) Value of a Superficial Portion of the Steel Sheet, KAM (C): KAM Value of a Central Portion of the Steel Sheet

This requirement is a highly important claim component in accordance with aspects of the present invention. The superficial portion of the steel sheet is located 100 μm below the steel sheet surface toward the center of the sheet thickness. The central portion of the steel sheet is located at ½ of the sheet thickness. Studies by the present inventors have revealed that varied distributions of dislocations from the superficial portion to the inside, specifically, KAM (S)/KAM (C) of less than 1.00 is effective for improving the YR and the range of appropriate clearances not leading to delayed fracture. Thus, KAM (S)/KAM (C) is limited to less than 1.00. The lower limit of KAM (S)/KAM (C) is not particularly limited but is preferably 0.80 or more due to production technology limitations.


Here, the KAM values are measured as follows. First, a test specimen for microstructure observation was sampled from the cold rolled steel sheet. Next, the sampled test specimen was polished by vibration polishing with colloidal silica to expose a cross section in the rolling direction (a longitudinal cross section) for use as observation surface. The observation surface was specular. Next, electron backscatter diffraction (EBSD) measurement was performed. Local crystal orientation data was thus obtained. Here, the SEM magnification was ×3000, the step size was 0.05 μm, the measured region was 20 μm square, and the WD was 15 mm. The local orientation data obtained was analyzed with analysis software: OIM Analysis 7. The analysis was performed with respect to 10 fields of view of the portion at the target sheet thickness, and the results were averaged.


Prior to the data analysis, cleanup was performed sequentially once using Grain Dilation function of the analysis software (Grain Tolerance Angle: 5, Minimum Grain Size: 2, Single Iteration: ON) and once with Grain CI Standardization function (Grain Tolerance Angle: 5, Minimum Grain Size: 5). Subsequently, measurement points with a CI value>0.1 were exclusively used for the analysis. The KAM values were displayed as a chart, and the average KAM value of the bcc phase was determined. The analysis here was performed under the following conditions:

    • Nearest neighbor: 1st,
    • Maximum misorientation: 5,
    • Perimeter only, and
    • Check Set 0-point kernels to maximum misorientation.








Hv

(
Q
)

-

Hv

(
S
)



8




Hv (Q): Hardness of a Portion at ¼ Sheet Thickness, Hv (S): Hardness of a Superficial Portion of the Steel Sheet

This requirement is a highly important claim component in accordance with aspects of the present invention. The superficial portion of the steel sheet is located 100 μm below the steel sheet surface toward the center of the sheet thickness. Studies by the present inventors have revealed that variations in hardness from the superficial portion to the inside, specifically, Hv (Q)-Hv (S) of 8 or more is effective for improving the YR and the range of appropriate clearances not leading to delayed fracture. Thus, Hv (Q)-Hv (S) is limited to 8 or more. The upper limit of Hv (Q)-Hv (S) is not particularly limited but is preferably 30 or less due to production technology limitations. Preferred ranges of Hv (Q) and Hv (S) are 400 to 600 and 400 to 600, respectively. Here, the hardness is measured as follows. First, a test specimen for microstructure observation was sampled from the cold rolled steel sheet. Next, the sampled test specimen was polished to expose a cross section in the rolling direction (a longitudinal cross section) for use as observation surface. The observation surface was specular. Next, the hardness was determined using a Vickers tester with a load of 1 kg. The hardness was measured with respect to 10 points at 20 μm intervals at the target sheet thickness. The values of 8 points excluding the maximum hardness and the minimum hardness were averaged.


Next, a manufacturing method according to aspects of the present invention will be described.


In accordance with aspects of the present invention, a steel material (a steel slab) may be obtained by any known steelmaking method without limitation, such as a converter or an electric arc furnace. To prevent macro-segregation, the steel slab (the slab) is preferably produced by a continuous casting method.


In accordance with aspects of the present invention, the slab heating temperature, the slab soaking holding time, and the coiling temperature in hot rolling are not particularly limited. For example, the steel slab may be hot rolled in such a manner that the slab is heated and is then rolled, that the slab is subjected to hot direct rolling after continuous casting without being heated, or that the slab is subjected to a short heat treatment after continuous casting and is then rolled. The slab heating temperature, the slab soaking holding time, the finish rolling temperature, and the coiling temperature in hot rolling are not particularly limited. The slab heating temperature is preferably 1100° C. or above. The slab heating temperature is preferably 1300° C. or below. The slab soaking holding time is preferably 30 minutes or more. The slab soaking holding time is preferably 250 minutes or less. The finish rolling temperature is preferably Ar3 transformation temperature or above. Furthermore, the coiling temperature is preferably 350° C. or above. The coiling temperature is preferably 650° C. or below.


The hot rolled steel sheet thus produced is pickled. Pickling can remove oxides on the steel sheet surface and is thus important to ensure good chemical convertibility and a high quality of coating in the final high strength steel sheet. Pickling may be performed at a time or several. The hot rolled sheet that has been pickled may be cold rolled directly or may be subjected to heat treatment before cold rolling.


The rolling reduction in cold rolling and the sheet thickness after rolling are not particularly limited. The rolling reduction in cold rolling is preferably 30% or more. The rolling reduction in cold rolling is preferably 80% or less. The advantageous effects according to aspects of the present invention may be obtained without limitations on the number of rolling passes and the rolling reduction in each pass.


The cold rolled steel sheet obtained as described above is annealed. Annealing conditions are as follows.


Annealing Temperature T1: 850° C. or Above and 1000° C. or Below

This requirement is a highly important claim component in accordance with aspects of the present invention. If the annealing temperature T1 is below 850° C., the area fraction of the total of ferrite and bainitic ferrite exceeds 10% to make it difficult to achieve 1320 MPa or higher TS and to achieve 85% or higher YR. Thus, the annealing temperature T1 is limited to 850° C. or above. T1 is preferably 860° C. or above. T1 is more preferably 870° C. or above. However, if the annealing temperature T1 is higher than 1000° C., the prior-austenite grain size excessively increases and the range of appropriate clearances not leading to delayed fracture is narrowed. Thus, the annealing temperature T1 is limited to 1000° C. or below. The annealing temperature T1 is preferably 970° C. or below. T1 is more preferably 950° C. or below.


Holding Time t1 at the Annealing Temperature T1: 10 Seconds or More and 1000 Seconds or Less

This requirement is a highly important claim component in accordance with aspects of the present invention. If the holding time t1 at the annealing temperature T1 is less than 10 seconds, austenitization is insufficient with the result that the area fraction of the total of ferrite and bainitic ferrite exceeds 10% to make it difficult to achieve 1320 MPa or higher TS and to achieve 85% or higher YR. Thus, the holding time t1 at the annealing temperature T1 is limited to 10 seconds or more. The holding time t1 at the annealing temperature T1 is preferably 30 seconds or more. t1 is more preferably 45 seconds or more. t1 is still more preferably 60 seconds or more. t1 is most preferably 100 seconds or more. However, if the holding time at the annealing temperature T1 is longer than 1000 seconds, the prior-austenite grain size excessively increases and the range of appropriate clearances not leading to delayed fracture is narrowed. Thus, the holding time t1 at the annealing temperature T1 is limited to 1000 seconds or less. The holding time t1 at the annealing temperature T1 is preferably 800 seconds or less. t1 is more preferably 500 seconds or less.


Cooling to 100° C. or Below after Annealing


In the step of cooling to 100° C. or below, austenite is transformed into martensite. To obtain 85% or more martensite, the annealed steel sheet needs to be cooled to 100° C. or below. Thus, cooling after annealing is effected to 100° C. or below. The lower limit of the cooling complete temperature is not particularly limited but is preferably 0° C. or above due to production technology limitations.


Elapsed Time t2 from the Time when the Temperature Reaches 100° C. Until the Start of Working: 1000 Seconds or Less


This requirement is a highly important claim component in accordance with aspects of the present invention. If the elapsed time t2 from the time when the temperature reaches 100° C. until the start of working is longer than 1000 seconds, aging of martensite microstructure proceeds and varied amounts of strains are introduced by working into the superficial portion of the steel sheet and the central portion of the steel sheet with the result that KAM (S)/KAM (C) becomes 1.00 or more. As a result, the YR is lowered and the range of appropriate clearances not leading to delayed fracture is narrowed. Thus, the elapsed time t2 from the time when the temperature reaches 100° C. until the start of working is limited to 1000 seconds or less. The elapsed time t2 from the time when the temperature reaches 100° C. until the start of working is preferably 900 seconds or less. t2 is more preferably 800 seconds or less. The lower limit of the elapsed time t2 from the time when the temperature reaches 100° C. until the start of working is not particularly limited but is preferably 5 seconds or more due to production technology limitations. Studies by the present inventors have shown that the elapsed time from the time when the temperature reaches 100° C. until the end of working does not affect the amounts of strains introduced by working into the superficial portion of the steel sheet and the central portion of the steel sheet.


Working Start Temperature T2: 80° C. or Below

This requirement is a highly important claim component in accordance with aspects of the present invention. If the working start temperature T2 is higher than 80° C., the steel sheet is soft and working introduces varied amounts of strains into the superficial portion of the steel sheet and the central portion of the steel sheet with the result that KAM (S)/KAM (C) becomes 1.00 or more. As a result, the YR is lowered and the range of appropriate clearances not leading to delayed fracture is narrowed. Thus, the working start temperature T2 is limited to 80° C. or below. The working start temperature T2 is preferably 60° C. or below. T2 is more preferably 50° C. or below. The lower limit of the working start temperature T2 is not particularly limited but is preferably 0° C. or above due to production technology limitations.


Equivalent Plastic Strain: 0.10% or More and 5.00% or Less

This requirement is a highly important claim component in accordance with aspects of the present invention. If the equivalent plastic strain is less than 0.10%, the amount of working is small and KAM (S)/KAM (C) becomes 1.00 or more. As a result, the YR is lowered and the range of appropriate clearances not leading to delayed fracture is narrowed. Thus, the equivalent plastic strain is limited to 0.10% or more. The equivalent plastic strain is preferably 0.15% or more. The equivalent plastic strain is more preferably 0.20% or more. If the equivalent plastic strain is more than 5.00%, the influences by working are equal between the superficial portion of the steel sheet and the central portion of the steel sheet with the result that KAM (S)/KAM (C) becomes 1.00 or more. As a result, the YR is lowered and the range of appropriate clearances not leading to delayed fracture is narrowed. The upper limit of the equivalent plastic strain is 5.00% or less due to production technology limitations. Thus, the equivalent plastic strain is limited to 5.00% or less. The equivalent plastic strain is preferably 4.00% or less. The equivalent plastic strain is more preferably 2.00% or less. The equivalent plastic strain is still more preferably 1.00% or less.


The working step before tempering is preferably performed under conditions where strain is applied by two or more separate working operations, and the total of the equivalent plastic strains applied in the working operations is 0.10% or more.


When the equivalent plastic strain in the first working operation is less than 0.108, the total of the equivalent plastic strains may be brought to 0.10% or more by the second and subsequent working operations. Even in this case, KAM (S)/KAM (C) becomes less than 1.00, and the YR and the range of appropriate clearances not leading to delayed fracture are enhanced. Thus, the working step before tempering may apply strain by two or more separate working operations as long as the total of the equivalent plastic strains applied in the working operations is 0.10% or more. Incidentally, there is no limitation on the elapsed time from when the temperature reaches 100° C. until the start of the second and subsequent working operations, because the mobility of dislocations in martensite has been lowered by the first working operation.


Here, the working process may be typically temper rolling or tension leveling. The equivalent plastic strain in temper rolling is the ratio by which the steel sheet is elongated and may be determined from the change in the length of the steel sheet before and after the working. The equivalent plastic strain of the steel sheet in leveler processing was calculated by the method of Reference 1 below. The data inputs described below were used in the calculation. Regarding the work hardening behavior, the material was assumed to be a linear hardening elastoplastic material. Bausinger hardening and the decrease in tension due to bend loss were ignored. Misaka's formula was used as the formula of bending curvature.

    • Sheet thickness breakdown: 31 divisions
    • Young's modulus: 21000 kgf/mm2
    • Poisson's ratio: 0.3
    • Yield stress: 111 kgf/mm2
    • Plastic coefficient: 1757 kgf/mm2
    • [Reference 1] Yoshisuke Misaka, Takeshi Masui; Sosei to Kakou (Journal of JSTP), 17 (1976), 988.


Incidentally, the working may be any common strain imparting technique other than those described above. For example, the working may be performed with a continuous stretcher leveler or a roller leveler.


Tempering Temperature T3: 100° C. or Above and 400° C. or Below

This requirement is a highly important claim component in accordance with aspects of the present invention. If the tempering temperature T3 is lower than 100° C., the carbon diffusion distance is so short that the hardness of the steel sheet surface and the inside of the steel sheet is lowered and Hv (Q)-Hv (S) becomes less than 8. As a result, the YR is lowered and the range of appropriate clearances not leading to delayed fracture is narrowed. Thus, the tempering temperature T3 is limited to 100° C. or above. The tempering temperature T3 is preferably 150° C. or above. T3 is more preferably 170° C. or above. T3 is still more preferably 200° C. or above. However, if the tempering temperature T3 is higher than 400° C., tempering of martensite proceeds to make it difficult to achieve 1320 MPa or higher TS. Thus, the tempering temperature T3 is limited to 400° C. or below. The tempering temperature T3 is preferably 350° C. or below. T3 is more preferably 300° C. or below. T3 is still more preferably 280° C. or below.


Holding Time t3 at the Tempering Temperature T3: 1.0 Second or More and 1000.0 Seconds or Less

This requirement is a highly important claim component in accordance with aspects of the present invention. If the holding time t3 at the tempering temperature T3 is less than 1.0 second, the carbon diffusion distance is so short that the hardness of the steel sheet surface and the inside of the steel sheet is lowered and Hv (Q)-Hv (S) becomes less than 8 with the result that the YR is lowered and the range of appropriate clearances not leading to delayed fracture is narrowed. Thus, the holding time t3 at the tempering temperature T3 is limited to 1.0 second or more. The holding time t3 at the tempering temperature T3 is preferably 5.0 seconds or more. t3 is more preferably 50.0 seconds or more. t3 is still more preferably 100.0 seconds or more. However, if the holding time t3 at the tempering temperature T3 is longer than 1000.0 seconds, tempering of martensite proceeds to make it difficult to achieve 1320 MPa or higher TS. Thus, the holding time t3 at the tempering temperature T3 is limited to 1000.0 seconds or less. The holding time t3 at the tempering temperature T3 is preferably 800.0 seconds or less. t3 is more preferably 600.0 seconds or less. t3 is still more preferably 500.0 seconds or less.


Cooling Rate 01 from the Tempering Temperature T3 to 80° C.: 100° C./Sec or Less


This requirement is a highly important claim component in accordance with aspects of the present invention. If the cooling rate 01 from the tempering temperature T3 to 80° C. is higher than 100° C./sec, the carbon diffusion distance is so short that the hardness of the steel sheet surface and the inside of the steel sheet is lowered and Hv (Q)-Hv (S) becomes less than 8 with the result that the YR is lowered and the range of appropriate clearances not leading to delayed fracture is narrowed. Thus, the cooling rate 01 from the tempering temperature T3 to 80° C. is limited to 100° C./sec or less. The cooling rate 01 from the tempering temperature T3 to 80° C. is preferably 50° C./sec or less. The lower limit of the cooling rate 01 from the tempering temperature T3 to 80° C. is not particularly limited but is preferably 10° C./sec or more due to production technology limitations.


Below 80° C., cooling is not particularly limited and the steel sheet may be cooled to a desired temperature in an appropriate manner. Incidentally, the desired temperature is preferably about room temperature.


Furthermore, the high strength steel sheet described above may be worked again under conditions where the amount of equivalent plastic strain is 0.10% or more and 5.00% or less. Here, the target amount of equivalent plastic strain may be applied at a time or several.


When the high strength steel sheet is a product that is traded, the steel sheet is usually traded after being cooled to room temperature.


The high strength steel sheet may be subjected to coating treatment during annealing or after annealing. The phrase “during annealing” means a period from the end of the holding time t1 at the annealing temperature T1 until when the steel sheet that has been held for t3 at the tempering temperature T3 is cooled to room temperature. The phrase “after annealing” means a period after the steel sheet is cooled to room temperature.


For example, the coating treatment during annealing may be hot-dip galvanizing treatment and alloying treatment following the hot-dip galvanizing treatment which are performed when the steel sheet that has been held at the annealing temperature T1 is being cooled to 100° C. or below. For example, the coating treatment after annealing may be Zn—Ni electrical alloying coating treatment or pure Zn electroplated coating treatment performed after the steel sheet that has been held for t3 at the tempering temperature T3 is cooled to room temperature. A coated layer may be formed by electroplated coating, or hot-dip zinc-aluminum-magnesium alloy coating may be applied. In the above coating treatment, examples were described focusing on zinc coating, the types of coating metals, such as Zn coating and Al coating, are not particularly limited. Other conditions in the manufacturing method are not particularly limited. From the point of view of productivity, the series of treatments including annealing, hot-dip galvanizing, and alloying treatment of the coated zinc layer is preferably performed on hot-dip galvanizing line, that is CGL (continuous galvanizing line). To control the coating weight of the coated layer, the hot-dip galvanizing treatment may be followed by wiping. Conditions for operations, such as coating, other than those conditions described above may be determined in accordance with the usual hot-dip galvanizing technique.


After the coating treatment during annealing or after annealing, the steel sheet may be worked again under conditions where the amount of equivalent plastic strain is 0.10% or more and 5.00% or less. Here, the target amount of equivalent plastic strain may be applied at a time or several.


EXAMPLES

Steels having a chemical composition described in Table 1-1 or Table 1-2, with the balance being Fe and incidental impurities, were smelted in a converter and were continuously cast into slabs. Next, the slabs obtained were heated, hot rolled, pickled, cold rolled, and subjected to annealing treatment, working, and tempering treatment described in Table 2-1, Table 2-2, and Table 2-3. High strength cold rolled steel sheets having a sheet thickness of 0.6 to 2.2 mm were thus obtained. Incidentally, some of the steel sheets were subjected to coating treatment after annealing.


In EXAMPLES Nos. 77, 82, 85, 88, and 91, the slabs fractured in the casting step and thus the test was discontinued.


The high strength cold rolled steel sheets obtained as described above were used as test steels. Tensile characteristics and delayed fracture resistance were evaluated in accordance with the following test methods.


(Microstructure Observation)

The area fraction of tempered martensite, the volume fraction of retained austenite, and the total of the area fraction of ferrite and the area fraction of bainitic ferrite were determined in accordance with the methods described hereinabove.


(KAM Values)

The KAM value of a superficial portion of the steel sheet and the KAM value of a central portion of the steel sheet were determined in accordance with the method described hereinabove.


(Hardness Test)

The hardness of a portion at ¼ Sheet Thickness and the hardness of a superficial portion of the steel sheet were determined in accordance with the method described hereinabove.


(Tensile Test)

A JIS No. 5 test specimen (gauge length: 50 mm, width of parallel portion: 25 mm) was sampled so that the longitudinal direction of the test specimen would be perpendicular to the rolling direction. A tensile test was performed in accordance with JIS Z 2241 under conditions where the crosshead speed was 1.67×10−1 mm/sec. YS and TS were thus measured. In accordance with aspects of the present invention, 1320 MPa or higher TS was judged to be acceptable, and 85% or higher yield ratio (YR) was judged to be acceptable. The YR is determined from the following formula (3):









YR
=

100
×
YS
/
TS





(
3
)







(Range of Appropriate Clearances not Leading to Delayed Fracture)

The range of appropriate clearances not leading to delayed fracture was determined by the following method. Test specimens having a size of 16 mm×75 mm were prepared by shearing in such a manner that the longitudinal direction would be perpendicular to the rolling direction. The rake angle in the shearing process was constant at 0°, and the shear clearance was changed from 5 to 10, 15, 20, 25, 30, and 35%. The test specimens were four-point loaded in accordance with ASTM (G39-99) so that 1000 MPa stress was applied to the bend apex. The loaded test specimens were immersed in pH 3 hydrochloric acid at 25° C. for 100 hours. The rating was “x” when the shear clearances that did not cause cracking ranged below 10%. The rating was “o” when the shear clearances ranged to 10% or above but below 158. The rating was “O” when the shear clearances that did not cause cracking ranged to 15% or above. The range of appropriate clearances not leading to delayed fracture was evaluated as excellent when the shear clearances that did not cause cracking ranged to 10% or above.


As described in Table 3-1, Table 3-2, and Table 3-3, INVENTIVE EXAMPLES achieved 1320 MPa or higher TS, 85% or higher YR, and an excellent range of appropriate clearances not leading to delayed fracture. In contrast, COMPARATIVE EXAMPLES were unsatisfactory in one or more of TS, YR, and the range of appropriate clearances not leading to delayed fracture.












TABLE 1-1









Chemical composition (mass %)






















Steels
C
Si
Mn
P
S
Al
N
H
Ti
B
Nb
Cu
Others
Remarks























A
0.21
0.71
2.96
0.010
0.0015
0.037
0.0018
0.0000
0.015



Compliant steel


B
0.20
0.90
3.02
0.011
0.0007
0.032
0.0068
0.0000




Compliant steel


C
0.20
0.85
2.89
0.005
0.0009
0.054
0.0023
0.0000

0.0015


Compliant steel


D
0.18
0.28
1.01
0.015
0.0008
0.047
0.0033
0.0000


0.005

Compliant steel


E
0.19
0.14
1.11
0.005
0.0013
0.012
0.0025
0.0000




Compliant steel


F
0.19
0.11
1.01
0.006
0.0011
0.057
0.0010
0.0000



0.11
Compliant steel


G
0.16
0.91
2.95
0.006
0.0015
0.023
0.0010
0.0000
0.041



Compliant steel



H


0.14

0.78
3.05
0.012
0.0006
0.045
0.0028
0.0000




Comparative steel


I
0.44
0.67
2.77
0.005
0.0006
0.034
0.0039
0.0000


0.016

Compliant steel



J


0.46

0.69
3.12
0.012
0.0005
0.012
0.0041
0.0000




Comparative steel


K
0.18
0.11
2.73
0.008
0.0012
0.025
0.0063
0.0000




Compliant steel


L
0.21
1.91
2.96
0.011
0.0008
0.011
0.0070
0.0000




Compliant steel



M

0.18

2.11

3.03
0.006
0.0008
0.036
0.0033
0.0000




Comparative steel


N
0.20
0.78
1.12
0.011
0.0006
0.015
0.0060
0.0000




Compliant steel



O

0.19
0.75

0.41

0.011
0.0007
0.026
0.0050
0.0000




Comparative steel


P
0.21
0.94
3.45
0.013
0.0006
0.044
0.0056
0.0000




Compliant steel



Q

0.20
0.77

3.55

0.009
0.0007
0.021
0.0070
0.0000




Comparative steel


R
0.20
0.70
3.02
0.099
0.0013
0.018
0.0066
0.0000




Compliant steel



S

0.19
0.61
2.78

0.121

0.0006
0.045
0.0031
0.0000




Comparative steel


T
0.21
0.67
3.04
0.006
0.0182
0.021
0.0030
0.0000




Compliant steel



U

0.22
0.94
2.96
0.012

0.0222

0.028
0.0048
0.0000




Comparative steel


V
0.19
0.99
2.84
0.010
0.0011
0.976
0.0029
0.0000




Compliant steel



W

0.18
0.67
2.76
0.015
0.0010

1.135

0.0015
0.0000




Comparative steel


X
0.22
0.85
3.16
0.006
0.0011
0.014
0.0089
0.0000




Compliant steel



Y

0.20
0.87
2.85
0.005
0.0009
0.027

0.0112

0.0000




Comparative steel


Z
0.21
0.84
2.98
0.014
0.0014
0.040
0.0046
0.0012




Compliant steel





Underlines indicate being outside of the range of the present invention. Blanks indicate that the element was not added intentionally.
















TABLE 1-2









Chemical composition (mass %)






















Steels
C
Si
Mn
P
S
Al
N
H
Ti
B
Nb
Cu
Others
Remarks

























AA

0.19
0.76
2.77
0.006
0.0007
0.056
0.0030

0.0035






Comparative steel


AB
0.21
0.91
2.96
0.005
0.0005
0.011
0.0033
0.0000

0.0028
0.019
0.15

Compliant steel


AC
0.21
0.64
3.01
0.006
0.0005
0.055
0.0038
0.0000
0.085
0.0022
0.029
0.18

Compliant steel



AD

0.20
0.81
2.82
0.010
0.0014
0.032
0.0062
0.0000

0.125

0.0017
0.028
0.12

Comparative steel


AE
0.19
0.89
3.15
0.010
0.0007
0.038
0.0032
0.0000
0.026

0.029
0.12

Compliant steel


AF
0.20
0.72
3.07
0.011
0.0013
0.010
0.0056
0.0000
0.021
0.0076
0.024
0.17

Compliant steel



AG

0.20
0.64
3.19
0.011
0.0012
0.016
0.0028
0.0000
0.045

0.0124

0.029
0.17

Comparative steel


AH
0.19
0.60
2.86
0.009
0.0007
0.015
0.0069
0.0000
0.019
0.0025

0.19

Compliant steel


AI
0.19
0.62
2.85
0.009
0.0011
0.034
0.0048
0.0000
0.030
0.0028
0.086
0.11

Compliant steel



AJ

0.19
0.89
3.16
0.009
0.0012
0.016
0.0047
0.0000
0.037
0.0014

0.135

0.12

Comparative steel


AK
0.22
0.68
3.11
0.007
0.0014
0.014
0.0018
0.0000
0.026
0.0018
0.025


Compliant steel


AL
0.18
0.62
2.83
0.007
0.0012
0.016
0.0022
0.0000
0.024
0.0026
0.026
0.96

Compliant steel



AM

0.21
0.79
2.99
0.015
0.0011
0.020
0.0042
0.0000
0.021
0.0026
0.012

1.02


Comparative steel


AN
0.19
0.22
1.33
0.010
0.0011
0.053
0.0047
0.0000




Cr: 0.340
Compliant steel


AO
0.21
0.83
2.86
0.013
0.0011
0.040
0.0011
0.0000




V: 0.056
Compliant steel


AP
0.21
0.18
1.00
0.014
0.0012
0.016
0.0035
0.0000




Mo: 0.330
Compliant steel


AQ
0.21
0.95
3.08
0.009
0.0008
0.011
0.0022
0.0000




Ni: 0.10
Compliant steel


AR
0.22
0.25
1.17
0.013
0.0013
0.056
0.0067
0.0000




As: 0.006
Compliant steel


AS
0.20
0.99
3.19
0.009
0.0006
0.047
0.0011
0.0000




Sb: 0.011
Compliant steel


AT
0.22
0.15
1.16
0.015
0.0006
0.031
0.0033
0.0000




Sn: 0.009
Compliant steel


AU
0.21
0.71
2.82
0.013
0.0009
0.022
0.0034
0.0000




Ta: 0.004
Compliant steel


AV
0.20
0.15
1.17
0.005
0.0008
0.017
0.0032
0.0000




Ca: 0.0014,
Compliant steel















Mg: 0.0150,















Zn: 0.006,















Co: 0.013


AW
0.21
0.61
2.79
0.008
0.0012
0.016
0.0062
0.0000




Zr: 0.0022
Compliant steel


AX
0.22
0.26
1.04
0.013
0.0006
0.059
0.0055
0.0000
0.044
0.0030
0.006
0.12
REM: 0.0150
Compliant steel


AY
0.17
0.15
1.03
0.013
0.0008
0.039
0.0049
0.0000





Compliant steel


AZ
0.33
0.28
1.30
0.008
0.0014
0.049
0.0063
0.0000





Compliant steel





Underlines indicate being outside of the range of the present invention. Blanks indicate that the element was not added intentionally.


























TABLE 2-1










Elapsed time t2





Cooling rate







An-

from when the
Working
Equiv-

Tem-

θ1 from




Sheet
nealing

temp. reached
start
alent

pering

tempering
Type




thick-
temp.
Holding
100° C. until
temp.
plastic
Working
temp.
Holding
temp. T3
of




ness
T1
time t1
start of working
T2
strain
operations
T3
time t3
to 80° C.
prod-


No.
Steels
(mm)
(° C.)
(sec)
(sec)
(° C.)
(%)
(times)
(° C.)
(sec)
(° C./sec)
uct (*)
Remarks




























1
A
1.4
875
105
729
44
0.44
1
237
160.5
29
CR
INV. EX.


2
B
1.4
870
151
653
25
0.55
1
250
 62.0
34
CR
INV. EX.


3
B
1.4
855
119
710
47
0.42
1
177
121.1
50
CR
INV. EX.


4
B
1.4

842

168
763
27
0.53
1
239
236.5
26
CR
COMP. EX.


5
B
1.4
968
155
731
41
0.50
1
176
248.2
36
CR
INV. EX.


6
B
1.4
989
133
653
42
0.40
1
260
176.5
28
CR
INV. EX.


7
B
1.4
874
 11
795
39
0.47
1
207
219.3
34
CR
INV. EX.


8
B
1.4
879
3
722
35
0.33
1
293
161.0
40
CR
COMP. EX.


9
B
1.4
878
956
777
47
0.35
1
266
236.0
49
CR
INV. EX.


10
B
1.4
868
992
711
47
0.32
1
198
263.7
34
CR
INV. EX.


11
B
1.4
875
106
 22
30
0.54
1
292
185.9
45
CR
INV. EX.


12
B
1.4
879
 71
723
27
0.37
2
215
294.1
50
CR
INV. EX.


13
B
1.4
874
179
986
48
0.39
1
211
276.5
34
CR
INV. EX.


14
B
1.4
860
146

1065

25
0.35
1
293
205.7
32
CR
COMP. EX.


15
B
1.4
862
 72
758
12
0.54
1
218
138.9
28
CR
INV. EX.


16
B
1.4
862
158
792
37
0.52
3
224
283.1
26
CR
INV. EX.


17
B
1.4
861
 56
730
77
0.44
1
150
217.0
41
CR
INV. EX.


18
B
1.4
877
 98
614

95

0.42
1
279
245.1
26
CR
COMP. EX.


19
B
1.4
880
107
683
32
0.13
1
180
243.4
32
CR
INV. EX.


20
B
1.4
879
160
670
48

0.08

1
246
258.0
48
CR
COMP. EX.


21
B
1.4
866
112
695
28
4.20
1
269
170.2
31
CR
INV. EX.


22
B
1.4
871
170
629
29
0.40
4
197
224.4
32
CR
INV. EX.


23
B
1.4
879
 83
652
35
0.54
1
106
200.6
30
CR
INV. EX.


24
B
1.4
865
151
612
33
0.39
1
90
228.7
31
CR
COMP. EX.


25
B
1.4
871
132
613
46
0.38
1
391
257.8
39
CR
INV. EX.


26
B
1.4
877
147
743
48
0.33
1
392
170.8
29
CR
INV. EX.


27
B
1.4
869
 58
668
49
0.57
1
275
 4.7
29
CR
INV. EX.


28
B
1.4
872
154
700
36
0.40
1
173
 2.2
45
CR
INV. EX.


29
B
1.4
866
101
709
27
0.58
1
292
 1.2
27
CR
INV. EX.


30
B
1.4
878
109
656
28
0.55
1
217
0.8
30
CR
COMP. EX.


31
B
1.4
879
180
690
48
0.34
1
232
988.0
38
CR
INV. EX.


32
B
1.4
872
175
725
28
0.54
1
200
998.5
49
CR
INV. EX.


33
B
1.4
879
151
610
45
0.58
1
218
146.7
5
CR
INV. EX.


34
B
1.4
870
 85
792
39
0.58
4
191
280.5
26
CR
INV. EX.


35
B
1.4
877
161
682
46
0.49
1
228
256.5
98
CR
INV. EX.





Underlines indicate being outside of the range of the present invention.


(*) CR: Cold rolled steel sheet (without coating)


























TABLE 2-2










Elapsed time t2





Cooling rate







An-

from when the
Working
Equiv-

Tem-

θ1 from




Sheet
nealing

temp. reached
start
alent

pering

tempering
Type




thick-
temp.
Holding
100° C. until
temp.
plastic
Working
temp.
Holding
temp. T3
of




ness
T1
time t1
start of working
T2
strain
operations
T3
time t3
to 80° C.
prod-


No.
Steels
(mm)
(° C.)
(sec)
(sec)
(° C.)
(%)
(times)
(° C.)
(sec)
(° C./sec)
uct (*)
Remarks




























36
B
1.4
872
58
706
29
0.52
1
204
228.1

125

CR
COMP. EX.


37
C
0.8
880
65
621
46
0.42
1
187
198.8
41
CR
INV. EX.


38
D
2.0
864
133
772
30
0.48
1
255
245.6
29
CR
INV. EX.


39
E
1.4
869
106
644
47
0.31
1
179
153.0
45
CR
INV. EX.


40
E
1.4
855
67
651
29
0.60
1
294
267.6
46
CR
INV. EX.


41
E
1.4
879
151
784
30
0.51
1
173
252.7
37
CR
INV. EX.


42
E
1.4
880
12
654
31
0.47
1
286
117.4
46
CR
INV. EX.


43
E
1.4
876
946
759
27
0.57
1
288
270.3
25
CR
INV. EX.


44
E
1.4
865
182
20
28
0.44
1
269
195.9
30
CR
INV. EX.


45
E
1.4
865
185
996
28
0.37
1
277
164.1
38
CR
INV. EX.


46
E
1.4
877
54
720
11
0.53
1
171
140.1
37
CR
INV. EX.


47
E
1.4
864
86
663
79
0.33
1
287
161.4
43
CR
INV. EX.


48
E
1.4
860
190
635
43
0.13
1
228
114.9
28
CR
INV. EX.


49
E
1.4
867
70
651
47
4.22
1
172
169.5
33
CR
INV. EX.


50
E
1.4
877
117
755
49
0.51
1
105
245.2
28
CR
INV. EX.


51
E
1.4
866
58
650
50
0.38
1
381
158.2
38
CR
INV. EX.


52
E
1.4
870
84
641
50
0.40
1
228
4.6
50
CR
INV. EX.


53
E
1.4
872
191
693
46
0.55
1
245
2.1
31
CR
INV. EX.


54
F
1.4
869
158
769
46
0.42
1
170
1.1
30
CR
INV. EX.


55
E
1.4
880
117
787
37
0.46
1
225
991.0
28
CR
INV. EX.


56
E
1.4
862
85
712
33
0.35
1
186
163.9
 4
CR
INV. EX.


57
E
1.4
877
157
748
30
0.49
1
296
240.2
88
CR
INV. EX.


58
F
1.2
861
132
602
44
0.42
1
274
198.2
40
CR
INV. EX.


59
G
1.2
874
149
697
32
0.43
1
253
135.5
29
GA
INV. EX.


60

H

1.2
874
116
722
49
0.36
1
222
231.8
44
GA
COMP. EX.


61
I
1.2
861
138
641
49
0.50
1
294
104.5
32
GA
INV. EX.


62

J

1.2
874
135
701
41
0.47
1
263
168.6
35
GA
COMP. EX.


63
K
1.2
865
125
757
28
0.56
1
221
147.9
41
GA
INV. EX.


64
L
1.2
867
103
774
38
0.31
1
253
185.8
45
CR
INV. EX.


65

M

1.2
864
126
651
36
0.56
1
152
121.6
37
CR
COMP. EX.


66
N
1.2
871
95
702
35
0.38
1
244
100.0
37
GA
INV. EX.


67

O

1.6
876
174
613
26
0.37
1
267
179.2
28
GA
COMP. EX.


68
P
1.6
861
52
621
35
0.51
1
196
202.4
47
G
INV. EX.


69

Q

1.6
873
158
672
48
0.50
1
278
181.0
27
GA
COMP. EX.


70
R
1.6
864
135
617
33
0.58
1
262
293.6
45
GA
INV. EX.





Underlines indicate being outside of the range of the present invention.


(*) CR: Cold rolled steel sheet (without coating), GI: Hot-dip galvanized steel sheet (without alloying treatment), GA: Galvannealed steel sheet


























TABLE 2-3










Elapsed time t2





Cooling rate







An-

from when the
Working
Equiv-

Tem-

θ1 from




Sheet
nealing

temp. reached
start
alent

pering

tempering
Type




thick-
temp.
Holding
100° C. until
temp.
plastic
Working
temp.
Holding
temp. T3
of




ness
T1
time t1
start of working
T2
strain
operations
T3
time t3
to 80° C.
prod-


No.
Steels
(mm)
(° C.)
(sec)
(sec)
(° C.)
(%)
(times)
(° C.)
(sec)
(° C./sec)
uct (*)
Remarks




























71

S

1.6
875
160
601
39
0.52
1
191
159.0
48
GA
COMP. EX.


72
T
1.6
878
72
623
41
0.33
1
233
169.5
37
GA
INV. EX.


73

U

1.6
878
182
742
28
0.55
1
222
156.0
29
GI
COMP. EX.


74
V
1.6
877
179
749
47
0.42
2
296
280.5
31
GA
INV. EX.


75

W

1.4
879
170
613
37
0.56
1
256
195.7
39
GA
COMP. EX.


76
X
1.4
870
51
759
36
0.37
1
159
156.5
28
GA
INV. EX.










77

Y

The slab fractured during casting and the test was discontinued.
COMP. EX.




















78
Z
1.4
869
76
727
34
0.38
1
164
201.6
47
GA
INV. EX.


79

AA

1.4
864
63
756
43
0.32
1
161
169.5
44
GI
COMP. EX.


80
AB
1.4
876
52
644
47
0.38
1
166
280.4
44
GA
INV. EX.


81
AC
1.4
864
78
765
49
0.56
1
182
175.5
32
GA
INV. EX.










82

AD

The slab fractured during casting and the test was discontinued.
COMP. EX.




















83
AE
1.4
871
123
757
37
0.58
1
276
233.2
29
GA
INV. EX.


84
AF
1.4
878
50
669
46
0.31
1
250
253.8
45
CR
INV. EX.










85

AG

The slab fractured during casting and the test was discontinued.
COMP. EX.




















86
AH
1.4
870
161
682
47
0.52
3
218
228.3
48
GA
INV. EX.


87
AI
1.4
860
181
628
48
0.52
1
273
125.0
28
GA
INV. EX.










88

AJ

The slab fractured during casting and the test was discontinued.
COMP. EX.




















89
AK
1.4
864
74
654
28
0.50
1
293
226.1
38
GA
INV. EX.


90
AL
1.4
860
173
730
50
0.46
1
223
289.8
41
GA
INV. EX.










91

AM

The slab fractured during casting and the test was discontinued.
COMP. EX.




















92
AN
1.4
864
193
641
33
0.39
1
199
246.6
43
GA
INV. EX.


93
AO
1.4
877
99
669
42
0.51
1
211
195.4
44
CR
INV. EX.


94
AP
1.4
879
161
731
42
0.48
1
285
260.8
44
CR
INV. EX.


95
AQ
1.4
863
105
681
35
0.44
1
167
194.5
28
CR
INV. EX.


96
AR
1.4
872
145
794
46
0.41
4
172
189.4
32
CR
INV. EX.


97
AS
1.4
869
156
788
32
0.57
1
251
293.6
49
CR
INV. EX.


98
AT
1.4
877
200
767
47
0.55
1
160
299.8
34
CR
INV. EX.


99
AU
1.4
870
107
681
43
0.55
4
225
293.9
45
CR
INV. EX.


100
AV
1.4
864
136
670
41
0.52
1
285
104.4
28
CR
INV. EX.


101
AW
1.4
876
60
664
29
0.41
1
262
221.4
33
CR
INV. EX.


102
AX
1.4
864
85
750
32
0.33
1
243
295.8
43
CR
INV. EX.


103
AY
0.8
879
195
693
31
0.39
1
211
272.2
45
EG
INV. EX.


104
AZ
2.0
879
136
669
33
0.36
1
180
109.4
42
EG
INV. EX.





Underlines indicate being outside of the range of the present invention.


(*) CR: Cold rolled steel sheet (without coating), GI: Hot-dip galvanized steel sheet (without alloying treatment), GA: Galvannealed steel sheet, EG: Electrogalvanized steel sheet






















TABLE 3-1









Sheet
Tempered
Retained
Total of ferrite and








thickness
martensite
austenite
bainitic ferrite
KAM(S)
KAM(C)
KAM(S)/


No.
Steels
(mm)
(%)
(%)
(%)
(°)
(°)
KAM(C)
Hv(Q)





1
A
1.4
98
2
0
0.504
0.536
0.941
516


2
B
1.4
99
1
0
0.501
0.538
0.931
508


3
B
1.4
91
1
8
0.508
0.535
0.949
473


4
B
1.4

83

3

14

0.499
0.531
0.940
414


5
B
1.4
99
1
0
0.514
0.541
0.950
548


6
B
1.4
99
1
0
0.502
0.534
0.940
511


7
B
1.4
90
1
9
0.505
0.537
0.939
458


8
B
1.4

83

2

15

0.516
0.537
0.960
391


9
B
1.4
99
1
0
0.510
0.537
0.950
503


10
B
1.4
100 
0
0
0.509
0.536
0.950
528


11
B
1.4
99
1
0
0.487
0.540
0.901
498


12
B
1.4
99
1
0
0.517
0.538
0.960
530


13
B
1.4
99
1
0
0.528
0.537
0.984
516


14
B
1.4
98
2
0
0.540
0.535

1.009

480


15
B
1.4
99
1
0
0.484
0.537
0.901
530


16
B
1.4
100 
0
0
0.505
0.537
0.941
522


17
B
1.4
100 
0
0
0.533
0.538
0.990
544


18
B
1.4
100 
0
0
0.541
0.538

1.004

481


19
B
1.4
99
1
0
0.532
0.541
0.984
538


20
B
1.4
100 
0
0
0.557
0.537

1.039

495


21
B
1.4
99
1
0
0.485
0.539
0.900
513


22
B
1.4
100 
0
0
0.509
0.536
0.950
538


23
B
1.4
99
1
0
0.499
0.537
0.930
475


24
B
1.4
99
1
0
0.504
0.536
0.941
526


25
B
1.4
99
1
0
0.510
0.537
0.950
473


26
B
1.4
100 
0
0
0.510
0.537
0.950
414


27
B
1.4
100 
0
0
0.502
0.533
0.940
530


28
B
1.4
99
1
0
0.512
0.533
0.960
523


29
B
1.4
98
2
0
0.491
0.533
0.920
520


30
B
1.4
99
1
0
0.502
0.541
0.929
519


31
B
1.4
99
1
0
0.514
0.535
0.960
474


32
B
1.4
99
1
0
0.506
0.539
0.940
423


33
B
1.4
99
1
0
0.503
0.535
0.941
535


34
B
1.4
98
2
0
0.507
0.540
0.940
539


35
B
1.4
98
2
0
0.506
0.539
0.940
519





















Hv(Q) −
YS
TS
YR
Range of appropriate clearances




No.
Hv(S)
Hv(S)
(MPa)
(MPa)
(%)
not leading to delayed fracture
Remarks







1
498
18
1451
1560
93

INV. EX.



2
491
17
1418
1538
92

INV. EX.



3
460
13
1235
1440
86

INV. EX.



4
395
19
1024
1240
83

COMP. EX.



5
534
14
1503
1674
90

INV. EX.



6
491
20
1455
1538
95

INV. EX.



7
441
17
1206
1384
87

INV. EX.



8
371
20
957
1159
83

COMP. EX.



9
483
20
1431
1513
95

INV. EX.



10
512
16
1467
1605
91

INV. EX.



11
472
26
1469
1478
99

INV. EX.



12
514
16
1471
1609
91

INV. EX.



13
506
10
1408
1585
89

INV. EX.



14
476
4
1218
1489
82
X
COMP. EX.



15
503
27
1561
1577
99

INV. EX.



16
503
19
1479
1577
94

INV. EX.



17
535
 9
1437
1675
86

INV. EX.



18
481
0
1186
1509
79
X
COMP. EX.



19
529
 9
1459
1659
88

INV. EX.



20
488
7
1290
1532
84
X
COMP. EX.



21
500
13
1350
1531
88

INV. EX.



22
523
15
1486
1640
91

INV. EX.



23
466
 9
1249
1459
86

INV. EX.



24
525
1
1309
1648
79
X
COMP. EX.



25
460
13
1180
1334
88

INV. EX.



26
395
19
1134
1331
85

INV. EX.



27
521
 9
1425
1633
87

INV. EX.



28
514
 9
1422
1610
88

INV. EX.



29
511
 9
1394
1601
87

INV. EX.



30
520

−1

1271
1634
78
X
COMP. EX.



31
449
25
1388
1408
99

INV. EX.



32
397
26
1238
1334
93

INV. EX.



33
511
24
1566
1601
98

INV. EX.



34
522
17
1506
1633
92

INV. EX.



35
509
10
1407
1596
88

INV. EX.







Underlines indicate being outside of the range of the present invention.






















TABLE 3-2









Sheet
Tempered
Retained
Total of ferrite and








thickness
martensite
austenite
bainitic ferrite
KAM(S)
KAM(C)
KAM(S)/


No.
Steels
(mm)
(%)
(%)
(%)
(°)
(°)
KAM(C)
Hv(Q)





36
B
1.4
100
0
0
0.507
0.540
0.940
523


37
C
0.8
98
2
0
0.503
0.535
0.941
529


38
D
2.0
99
1
0
0.504
0.536
0.941
509


39
E
1.4
98
2
0
0.517
0.538
0.960
546


40
E
1.4
92
1
7
0.498
0.536
0.930
447


41
E
1.4
98
2
0
0.506
0.539
0.940
548


42
E
1.4
91
1
8
0.502
0.534
0.940
447


43
E
1.4
99
1
0
0.499
0.537
0.930
498


44
E
1.4
99
1
0
0.487
0.540
0.901
507


45
E
1.4
98
2
0
0.529
0.538
0.984
488


46
E
1.4
98
2
0
0.482
0.535
0.900
565


47
E
1.4
99
1
0
0.525
0.534
0.982
485


48
E
1.4
99
1
0
0.529
0.539
0.982
511


49
E
1.4
99
1
0
0.485
0.538
0.901
564


50
E
1.4
99
1
0
0.502
0.534
0.940
525


51
E
1.4
99
1
0
0.509
0.536
0.950
453


52
E
1.4
100
0
0
0.518
0.539
0.960
525


53
E
1.4
99
1
0
0.502
0.533
0.940
526


54
E
1.4
98
2
0
0.508
0.535
0.949
530


55
E
1.4
100
0
0
0.505
0.537
0.939
454


56
E
1.4
100
0
0
0.518
0.540
0.960
546


57
E
1.4
98
2
0
0.504
0.536
0.941
486


58
F
1.2
99
1
0
0.505
0.537
0.939
502


59
G
1.2
100
0
0
0.510
0.537
0.950
443


60

H

1.2
99
1
0
0.510
0.531
0.960
414


61
I
1.2
99
1
0
0.506
0.539
0.940
604


62

J

1.2
100
0
0
0.507
0.534
0.949
595


63
K
1.2
99
1
0
0.498
0.535
0.930
460


64
L
1.2
96
4
0
0.510
0.537
0.950
514


65

M

1.2
94

6

0
0.505
0.537
0.941
544


66
N
1.2
91
0
9
0.510
0.537
0.950
462


67

O

1.6
85
4

11

0.517
0.538
0.960
362


68
P
1.6
98
2
0
0.504
0.536
0.941
544


69

Q

1.6
98
2
0
0.502
0.534
0.940
504


70
R
1.6
99
1
0
0.506
0.538
0.939
503





















Hv(Q) −
YS
TS
YR
Range of appropriate clearances




No.
Hv(S)
Hv(S)
(MPa)
(MPa)
(%)
not leading to delayed fracture
Remarks







36
521
2
1309
1632
80
X
COMP. EX.



37
514
15
1457
1608
91

INV. EX.



38
488
21
1460
1530
95

INV. EX.



39
534
12
1473
1670
88

INV. EX.



40
425
22
1137
1333
85

INV. EX.



41
533
15
1516
1673
91

INV. EX.



42
427
20
1141
1337
85

INV. EX.



43
476
22
1438
1495
96

INV. EX.



44
482
25
1489
1510
99

INV. EX.



45
478
10
1291
1497
86

INV. EX.



46
538
27
1669
1686
99

INV. EX.



47
477
 8
1323
1498
88

INV. EX.



48
502
 9
1383
1571
88

INV. EX.



49
538
26
1676
1686
99

INV. EX.



50
516
 9
1414
1614
88

INV. EX.



51
444
 9
1192
1390
86

INV. EX.



52
516
 9
1394
1616
86

INV. EX.



53
517
 9
1425
1620
88

INV. EX.



54
520
10
1405
1633
86

INV. EX.



55
431
23
1311
1352
97

INV. EX.



56
522
24
1601
1637
98

INV. EX.



57
478
 8
1304
1500
87

INV. EX.



58
481
21
1439
1508
95

INV. EX.



59
425
18
1239
1332
93

INV. EX.



60
398
16
1141
1248
91

COMP. EX.



61
584
20
1731
1830
95

INV. EX.



62
576
19
1692
1804
94
X
COMP. EX.



63
442
18
1289
1386
93

INV. EX.



64
495
19
1327
1551
86

INV. EX.



65
532
12
1365
1665
82

COMP. EX.



66
446
16
1216
1397
87

INV. EX.



67
344
18
907
1077
84

COMP. EX.



68
528
16
1511
1653
91

INV. EX.



69
483
21
1447
1517
95
X
COMP. EX.



70
481
22
1452
1509
96

INV. EX.







Underlines indicate being outside of the range of the present invention.






















TABLE 3-3









Sheet
Tempered
Retained
Total of ferrite and








thickness
martensite
austenite
bainitic ferrite
KAM(S)
KAM(C)
KAM(S)/


No.
Steels
(mm)
(%)
(%)
(%)
(°)
(°)
KAM(C)
Hv(Q)





71

S

1.6
98
2
0
0.497
0.534
0.930
525


72
T
1.6
98
2
0
0.510
0.537
0.950
508


73

U

1.6
99
1
0
0.498
0.536
0.930
529


74
V
1.6
90
1
9
0.514
0.536
0.960
445


75

W

1.4
88
2
10
0.504
0.536
0.941
436


76
X
1.4
99
1
0
0.512
0.533
0.960
556









77

Y

The slab fractured during casting and the test was discontinued.
















78
Z
1.4
98
2
0
0.514
0.536
0.960
545


79

AA

1.4
98
2
0
0.514
0.536
0.960
535


80
AB
1.4
98
2
0
0.511
0.538
0.950
461


81
AC
1.4
99
1
0
0.502
0.534
0.940
597









82

AD

The slab fractured during casting and the test was discontinued.
















83
AE
1.4
99
1
0
0.495
0.533
0.930
471


84
AF
1.4
100
0
0
0.512
0.539
0.950
607









85

AG

The slab fractured during casting and the test was discontinued.
















86
AH
1.4
99
1
0
0.507
0.540
0.940
484


87
AI
1.4
99
1
0
0.514
0.541
0.950
606









88

AJ

The slab fractured during casting and the test was discontinued.
















89
AK
1.4
100
0
0
0.498
0.536
0.930
497


90
AL
1.4
100
0
0
0.502
0.533
0.940
503









91

AM

The slab fractured during casting and the test was discontinued.
















92
AN
1.4
99
1
0
0.502
0.533
0.940
540


93
AO
1.4
99
1
0
0.505
0.537
0.941
527


94
AP
1.4
98
2
0
0.506
0.539
0.940
506


95
AQ
1.4
98
2
0
0.511
0.538
0.950
553


96
AR
1.4
99
1
0
0.506
0.538
0.939
557


97
AS
1.4
99
1
0
0.497
0.534
0.930
524


98
AT
1.4
100
0
0
0.506
0.539
0.940
562


99
AU
1.4
98
2
0
0.503
0.535
0.941
521


100
AV
1.4
98
2
0
0.504
0.536
0.941
500


101
AW
1.4
99
1
0
0.504
0.536
0.941
505


102
AX
1.4
98
2
0
0.509
0.536
0.950
526


103
AY
0.8
100
0
0
0.506
0.533
0.949
470


104
AZ
2.0
98
2
0
0.515
0.537
0.960
592





















Hv(Q) −
YS
TS
YR
Range of appropriate clearances




No.
Hv(S)
Hv(S)
(MPa)
(MPa)
(%)
not leading to delayed fracture
Remarks







71
509
16
1460
1597
91
X
COMP. EX.



72
491
17
1420
1540
92

INV. EX.



73
511
18
1490
1602
93
X
COMP. EX.



74
423
22
1178
1324
89

INV. EX.



75
416
20
1044
1305
80

COMP. EX.



76
544
12
1502
1703
88

INV. EX.











77
The slab fractured during casting and the test was discontinued.
COMP. EX.
















78
533
12
1469
1666
88

INV. EX.



79
523
12
1448
1642
88
X
COMP. EX.



80
447
14
1259
1402
90

INV. EX.



81
582
15
1651
1822
91

INV. EX.











82
The slab fractured during casting and the test was discontinued.
COMP. EX.
















83
449
22
1352
1405
96

INV. EX.



84
588
19
1732
1846
94

INV. EX.











85
The slab fractured during casting and the test was discontinued.
COMP. EX.
















86
466
18
1357
1459
93

INV. EX.



87
587
19
1727
1841
94

INV. EX.











88
The slab fractured during casting and the test was discontinued.
COMP. EX.
















89
475
22
1434
1491
96

INV. EX.



90
484
19
1424
1518
94

INV. EX.











91
The slab fractured during casting and the test was discontinued.
COMP. EX.
















92
523
17
1508
1636
92

INV. EX.



93
510
17
1472
1597
92

INV. EX.



94
484
22
1456
1513
96

INV. EX.



95
540
13
1505
1691
89

INV. EX.



96
543
14
1526
1699
90

INV. EX.



97
502
22
1512
1572
96

INV. EX.



98
548
14
1543
1718
90

INV. EX.



99
502
19
1475
1573
94

INV. EX.



100
480
20
1425
1506
95

INV. EX.



101
484
21
1443
1513
95

INV. EX.



102
507
19
1490
1589
94

INV. EX.



103
453
17
1306
1416
92

INV. EX.



104
580
12
1606
1821
88

INV. EX.







Underlines indicate being outside of the range of the present invention.





Claims
  • 1. A high strength steel sheet comprising a microstructure having a chemical composition comprising, by mass %: C: 0.15% or more and 0.45% or less,Si: 0.10% or more and 2.00% or less,Mn: 0.5% or more and 3.5% or less,P: 0.100% or less,S: 0.0200% or less,Al: 0.010% or more and 1.000% or less,N: 0.0100% or less, andH: 0.0020% or less,the balance being Fe and incidental impurities;the microstructure being such that:the area fraction of tempered martensite is 85% or more,the volume fraction of retained austenite is less than 5%, andthe area fraction of the total of ferrite and bainitic ferrite is 10% or less;the microstructure satisfying formulas (1) and (2) defined below:
  • 2. The high strength steel sheet according to claim 1, wherein the chemical composition further comprises one, or two or more elements selected from, by mass %: Ti: 0.100% or less,B: 0.0100% or less,Nb: 0.100% or less,Cu: 1.00% or less,Cr: 1.00% or less,V: 0.100% or less,Mo: 0.500% or less,Ni: 0.50% or less,Sb: 0.200% or less,Sn: 0.200% or less,As: 0.100% or less,Ta: 0.100% or less,Ca: 0.0200% or less,Mg: 0.0200% or less,Zn: 0.020% or less,Co: 0.020% or less,Zr: 0.020% or less, andREM: 0.0200% or less.
  • 3. The high strength steel sheet according to claim 1, which has a coated layer on a surface of the steel sheet.
  • 4. The high strength steel sheet according to claim 2, which has a coated layer on a surface of the steel sheet.
  • 5. A method for manufacturing a high strength steel sheet described in claim 1, the method comprising: providing a cold rolled steel sheet produced by subjecting a steel slab to hot rolling, pickling, and cold rolling;annealing the steel sheet under conditions where:a temperature T1 is 850° C. or above and 1000° C. or below anda holding time t1 at T1 is 10 seconds or more and 1000 seconds or less;cooling the steel sheet to 100° C. or below;starting working at an elapsed time t2 of 1000 seconds or less from the time when the temperature reaches 100° C.,the working being performed under conditions where:a working start temperature T2 is 80° C. or below andan equivalent plastic strain is 0.10% or more and 5.00% or less;tempering the steel sheet under conditions where:a temperature T3 is 100° C. or above and 400° C. or below anda holding time t3 at T3 is 1.0 second or more and 1000.0 seconds or less; andcooling the steel sheet under conditions where a cooling rate 01 from T3 to 80° C. is 100° C./sec or less.
  • 6. A method for manufacturing a high strength steel sheet described in claim 2, the method comprising: providing a cold rolled steel sheet produced by subjecting a steel slab to hot rolling, pickling, and cold rolling;annealing the steel sheet under conditions where:a temperature T1 is 850° C. or above and 1000° C. or below anda holding time t1 at T1 is 10 seconds or more and 1000 seconds or less;cooling the steel sheet to 100° C. or below;starting working at an elapsed time t2 of 1000 seconds or less from the time when the temperature reaches 100° C.,the working being performed under conditions where:a working start temperature T2 is 80° C. or below andan equivalent plastic strain is 0.10% or more and 5.00% or less;tempering the steel sheet under conditions where:a temperature T3 is 100° C. or above and 400° C. or below anda holding time t3 at T3 is 1.0 second or more and 1000.0 seconds or less; andcooling the steel sheet under conditions where a cooling rate 01 from T3 to 80° C. is 100° C./sec or less.
  • 7. The method for manufacturing a high strength steel sheet according to claim 5, wherein the working before the tempering is performed under conditions where strain is applied by two or more separate working operations, and the total of the equivalent plastic strains applied in the working operations is 0.10% or more.
  • 8. The method for manufacturing a high strength steel sheet according to claim 6, wherein the working before the tempering is performed under conditions where strain is applied by two or more separate working operations, and the total of the equivalent plastic strains applied in the working operations is 0.10% or more.
  • 9. The method for manufacturing a high strength steel sheet according to claim 5, further comprising performing coating treatment during the annealing or after the annealing.
  • 10. The method for manufacturing a high strength steel sheet according to claim 6, further comprising performing coating treatment during the annealing or after the annealing.
  • 11. The method for manufacturing a high strength steel sheet according to claim 7, further comprising performing coating treatment during the annealing or after the annealing.
  • 12. The method for manufacturing a high strength steel sheet according to claim 8, further comprising performing coating treatment during the annealing or after the annealing.
Priority Claims (1)
Number Date Country Kind
2021-098034 Jun 2021 JP national
CROSS REFERENCE TO RELATED APPLICATIONS

This is the U.S. National Phase Application of PCT/JP2022/020892, filed May 19, 2022, which claims priority to Japanese Patent Application No. 2021-098034, filed Jun. 11, 2021, the disclosures of these applications being incorporated herein by reference in their entireties for all purposes.

PCT Information
Filing Document Filing Date Country Kind
PCT/JP2022/020892 5/19/2022 WO