HIGH STRENGTH STEEL SHEET, HIGH STRENGTH COATED OR PLATED STEEL SHEET, METHODS OF PRODUCING THESE, AND MEMBER

Abstract
The steel sheet comprising a chemical composition containing C, Si, Mn, P, S, Al, N, Ti, Nb, and B, with the balance being Fe and inevitable impurities, and satisfying predetermined formula, in which the total area ratio of martensite and bainite is 95% or more, the average grain size of prior austenite grains is 10 μm or less, the B concentration at a prior austenite grain boundary is 0.10% or more in mass %, a C-concentrated region is provided along a martensitic grain boundary, and the C-concentrated region has a C concentration of 4.0 times or more than the C content in the steel, and the C-concentrated region has a concentration width of 3 nm or more and 100 nm or less in a direction perpendicular to the martensitic grain boundary and a length of 100 nm or more in a direction parallel to the martensitic grain boundary.
Description
TECHNICAL FIELD

The present disclosure relates to a high strength steel sheet, a method of producing the same, and a member.


BACKGROUND

Automotive steel sheets are required to have higher strength to improve fuel efficiency by reducing the weight of the automotive body. High strength steel sheets with a tensile strength of 1180 MPa or higher are required for frame parts. In addition, high bendability is required for steel sheets to be subjected to press working and formed into desired shapes. Furthermore, from the viewpoint of crashworthiness of automobiles, there are some automotive parts required not to easily deform to ensure driver's and passenger's living space during a collision, in addition to strength. The use of steel sheets with a high yield ratio is desirable for such automotive parts. In addition, high toughness is required to ensure that automotive parts do not fracture in a collision.


JP5728108B (PTL 1) discloses a high strength steel sheet with excellent formability and low-temperature toughness and a method of producing the same. JP6597939B (PTL 2) discloses a high strength steel sheet with excellent formability and anti-crash property, and a method of producing a high strength steel sheet with excellent formability and anti-crash property. JP6700398B (PTL 3) discloses a high yield ratio type high strength steel sheet and a method of producing the same.


CITATION LIST
Patent Literature





    • PTL 1: JP5728108B

    • PTL 2: JP6597939B

    • PTL 3: JP6700398B





SUMMARY
Technical Problem

However, the yield ratio is not considered in PTLs 1 and 2. Toughness is not considered in PTL 3.


As described above, it is difficult to produce a high strength steel sheet with a tensile strength of 1180 MPa or higher, excellent bendability and toughness, and a high yield ratio using conventional techniques.


This disclosure has been made in view of these circumstances. It could be helpful to provide a high strength steel sheet with a tensile strength of 1180 MPa or higher, excellent bendability and toughness, and a high yield ratio, and a method of producing the same.


In this disclosure, high strength means that a tensile strength TS measured in accordance with JIS Z2241 is 1180 MPa or higher.


Excellent bendability means that a bending test specimen does not crack at the ridge of a tip thereof in a bend test conducted in accordance with JIS Z2248.


Excellent toughness means that the brittle-ductile transition temperature is −40° C. or lower in a Charpy impact test conducted in accordance with JIS Z2242.


A high yield ratio means that a ratio YS/TS of yield stress to tensile strength measured in accordance with JIS Z2241 is 0.80 or more.


Solution to Problem

We conducted diligent studies to accomplish the above-mentioned tasks and discovered the following.


(1) Crack initiation and propagation during bending and a fracture path during brittle fracture are along the prior austenite grain boundary. Therefore, refining crystal grains to complicate the fracture path and increasing the strength of the grain boundary are effective in improving bendability. To refine prior austenite grains, it is effective to keep the annealing temperature as low as possible at a temperature equal to or higher than 850° C., which is an austenite single phase region. On the other hand, grain boundary segregation of B is effective in strengthening the grain boundary, but the grain boundary segregation amount of B increases as being annealed at higher temperature.


Therefore, to increase the grain boundary segregation amount of B while maintaining fine crystal grain size, annealing is performed at around 850° C. to obtain fine austenite grains, followed by rapid heating and rapid cooling. This promotes grain boundary segregation of B by diffusion while inhibiting crystal grain growth, thereby simultaneously achieving austenite grain size refinement and grain boundary segregation of B.


(2) Dislocations present in quenched martensitic microstructure are mobile dislocations that easily generate sliding motion at low stresses, resulting in low yield stresses in the martensitic microstructure. However, when the steel sheet after quenching is slightly processed, these dislocations move close to the grain boundary, where they become entangled and form immobile dislocations. This can increase the yield ratio of the steel sheet.


(3) Tempering the steel sheet at low temperatures causes carbon segregation on dislocations or cluster precipitation. Tempering at low temperatures the steel sheet after processing, in which dislocations are accumulated near the crystal grain boundary, forms a region of high C concentration (C-concentrated region) on the network along the grain boundary, which significantly increases the strength near the grain boundary. Since C is concentrated not only in the grain boundary but also in the matrix phases sandwiching the grain boundary, its strength-increasing effect is extremely large. Since the grain boundary is not easily deformed, the yield ratio also increases significantly due to the formation of the C-concentrated region.


This disclosure is based on the aforementioned discoveries and primary features thereof are described below.


[1] A high strength steel sheet comprising a chemical composition containing (consisting of), in mass %:

    • C: 0.10% or more and 0.30% or less;
    • Si: 0.20% or more and 1.20% or less;
    • Mn: 2.5% or more and 4.0% or less;
    • P: 0.050% or less;
    • S: 0.020% or less;
    • Al: 0.10% or less;
    • N: 0.01% or less;
    • Ti: 0.100% or less;
    • Nb: 0.002% or more and 0.050% or less; and
    • B: 0.0005% or more and 0.0050% or less,


      with the balance being Fe and inevitable impurities, and satisfying the following formula (1), wherein
    • the total area ratio of martensite and bainite is 95% or more,
    • the average grain size of prior austenite grains is 10 μm or less,
    • the B concentration at a prior austenite grain boundary is 0.10% or more in mass %,
    • a C-concentrated region is provided along a martensitic grain boundary,
    • the C concentration in the C-concentrated region is 4.0 times or more than the C content in the steel, and
    • the C-concentrated region has a concentration width of 3 nm or more and 100 nm or less in a direction perpendicular to the martensitic grain boundary and a length of 100 nm or more in a direction parallel to the martensitic grain boundary:












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in the formula (1), [% N] and [% Ti] indicate the N content and the Ti content in the steel in mass %, respectively.


[2] The high strength steel sheet according to [1] above, wherein the chemical composition further contains at least one element selected from, in mass %:

    • V: 0.100% or less;
    • Mo: 0.500% or less;
    • Cr: 1.00% or less;
    • Cu: 1.00% or less;
    • Ni: 0.50% or less;
    • Sb: 0.200% or less;
    • Sn: 0.200% or less;
    • Ta: 0.200% or less;
    • W: 0.400% or less;
    • Zr: 0.0200% or less;
    • Ca: 0.0200% or less;
    • Mg: 0.0200% or less;
    • Co: 0.020% or less;
    • REM: 0.0200% or less;
    • Te: 0.020% or less;
    • Hf: 0.10% or less; or
    • Bi: 0.200% or less.


[3] A high strength coated or plated steel sheet having a coated or plated layer on at least one surface of the high strength steel sheet according to [1] or [2] above.


[4] A method of producing a high strength steel sheet, comprising:

    • hot rolling a steel slab having the chemical composition according to [1] or [2] above to form a hot-rolled sheet;
    • cold rolling the hot-rolled sheet to form a cold-rolled sheet;
    • performing an annealing process in which the cold-rolled sheet is heated to a first heating temperature of 850° C. or higher and 920° C. or lower and held for 10 seconds or longer, the temperature is then raised to a second heating temperature of 1000° C. or higher and 1200° C. or lower at an average heating rate of 50° C./s or more, and the sheet is cooled to 500° C. or lower at an average cooling rate of 50° C./s or more within 5 seconds after reaching the second heating temperature,
    • after the annealing process, performing a rolling process in which the cold-rolled sheet is rolled at an elongation rate of 0.5% or more to obtain a second cold-rolled sheet, and
    • after the rolling process, performing a reheating process in which the second cold-rolled sheet is held at a reheating temperature of 70° C. or higher and 200° C. or lower for 600 seconds or longer to obtain a high strength steel sheet.


[5] A method of producing a high strength coated or plated steel sheet, comprising a coating or plating process in which, after the annealing process according to [4] above and before the reheating process, at least one surface of the high strength steel sheet is subjected to coating or plating treatment to obtain a high strength coated or plated steel sheet.


[6] A member formed using the high strength steel sheet according to [1] or [2] above for at least a portion thereof.


[7] A member formed using the high strength coated or plated steel sheet according to [3] above for at least a portion thereof.


Advantageous Effect

According to this disclosure, it is possible to provide a high strength steel sheet with a tensile strength of 1180 MPa or higher, excellent bendability and toughness, and a high yield ratio, and a method of producing the same.





BRIEF DESCRIPTION OF THE DRAWINGS

In the accompanying drawings:



FIG. 1A and FIG. 1B are drawings illustrating an example of C-concentrated regions.





DETAILED DESCRIPTION

The following describes embodiments of the present disclosure. However, this disclosure is not limited to the following embodiments. First, description will be made on the appropriate range of the chemical composition of steel sheets and the reasons for its limitation. The “%” representations below indicating the chemical composition of the steel sheet are in “mass %” unless stated otherwise. In the present specification, a numerical range expressed by using “to” means a range including numerical values described before and after “to”, as the lower limit value and the upper limit value.


C: 0.10% or More and 0.30% or Less

In addition to strengthening the martensitic microstructure and bainitic microstructure, C has the effect of strengthening the grain boundary by segregating at dislocations accumulated near the prior austenite grain boundary, thereby increasing bendability, toughness, and yield ratio. When the C content is less than 0.10%, the area ratios of martensite and bainite decrease, and a TS of 1180 MPa or higher cannot be obtained. When the C content exceeds 0.30%, carbon borides with B and iron are formed during annealing, and a sufficient amount of B cannot be segregated at the prior austenite grain boundary. The C content is preferably 0.11% or more. The C content is preferably 0.28% or less.


Si: 0.20% or More and 1.20% or Less

Si is an element effective for solid solution strengthening and requires an addition of 0.20% or more. On the other hand, Si is an element that stabilizes ferrite and raises the transformation temperature. Therefore, when the Si content exceeds 1.20%, it is difficult to make the prior austenite grain size 10 μm or less. The Si content is preferably 0.50% or more. The Si content is preferably 1.10% or less.


Mn: 2.5% or More and 4.0% or Less

Mn is effective in improving hardenability. When the Mn content is less than 2.5%, the area ratios of martensite and bainite decrease, resulting in lower strength. On the other hand, when the Mn content exceeds 4.0%, the segregated portions are excessively hardened, resulting in lower bendability. The Mn content is preferably 2.8% or more. The Mn content is preferably 3.5% or less.


P: 0.050% or Less

The P content is 0.050% or less because P segregates at the prior austenite grain boundary and reduces toughness. No particular lower limit is placed on the P content, which may be 0%. However, the P content is preferably 0.001% or more because a P content of less than 0.001% increases the production cost. The P content is preferably 0.025% or less.


S: 0.020% or Less

The S content is 0.020% or less because S segregates at the prior austenite grain boundary and reduces toughness. No particular lower limit is placed on the S content. However, the S content is preferably 0.0001% or more because a S content of less than 0.0001% increases the production cost. The S content is preferably 0.018% or less.


Al: 0.10% or Less

Al is an element that acts as a deoxidizing material. To obtain such an effect, the Al content is preferably 0.005% or more. On the other hand, when the Al content exceeds 0.10%, ferrite is easily generated, and strength is reduced. The Al content is preferably 0.05% or less.


N: 0.01% or Less

N forms nitrides with Nb and B, reducing the effect of Nb and B addition. Therefore, the N content is 0.01% or less. No particular lower limit is placed on the N content. However, from the viewpoint of production cost, the N content is preferably 0.0001% or more.


Ti: 0.100% or Less

Ti has the effect of fixing N in steel as TiN and inhibiting the generation of BN and NbN. To achieve these effects, the Ti content is preferably 0.005% or more. On the other hand, when the Ti content exceeds 0.100%, coarse Ti carbides are formed on the grain boundary, and toughness is reduced. The Ti content is preferably 0.05% or less.


Nb: 0.002% or More and 0.050% or Less

Nb precipitates as a solute or fine carbides and inhibits the growth of austenite grains during annealing. To achieve such an effect, the Nb content is 0.002% or more. On the other hand, when the Nb content exceeds 0.050%, not only does the effect saturate, but coarse Nb carbides precipitate and the toughness is reduced. The Nb content is preferably 0.005% or more. The Nb content is preferably 0.040% or less.


B: 0.0005% or More and 0.0050% or Less

B segregates at the prior austenite grain boundary and has the effect of increasing grain boundary strength. To achieve such an effect, the B content is 0.0005% or more. On the other hand, when the B content exceeds 0.0050%, carbon borides are formed, and toughness is reduced. The B content is preferably 0.0010% or more. The B content is preferably 0.0030% or less.











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To achieve the above-described effect of B and Nb addition, N, which readily combines with these elements, needs to be fixed by Ti. Therefore, the mole fraction of N is set to be smaller than the mole fraction of Ti. In other words, the N content and the Ti content in the steel are adjusted to satisfy the above formula (1). In the formula (1), [% N] and [% Ti] indicate the N content and the Ti content in the steel (mass %), respectively.


[Optional Component]

The high strength cold-rolled steel sheet according to the embodiment may further contain at least one element selected from, in mass %: V: 0.100% or less; Mo: 0.500% or less; Cr: 1.00% or less; Cu: 1.00% or less; Ni: 0.50% or less; Sb: 0.200% or less; Sn: 0.200% or less; Ta: 0.200% or less; W: 0.400% or less; Zr: 0.0200% or less; Ca: 0.0200% or less; Mg: 0.0200% or less; Co: 0.020% or less; REM: 0.0200% or less; Te: 0.020% or less; Hf: 0.10% or less; or Bi: 0.200% or less, in addition to the above-described chemical composition.


V: 0.100% or Less

V has the effect of forming fine carbides and increasing strength. When the V content exceeds 0.100%, coarse V carbides precipitate, and toughness is reduced. No particular lower limit is placed on the V content, which may be 0.000%. However, the V content is preferably 0.001% or more because V has the effect of forming fine carbides and increasing strength.


Mo: 0.500% or Less

Mo has the effect of improving hardenability and increasing the fractions of bainite and martensite. When the Mo content exceeds 0.500%, the effect is saturated. No particular lower limit is placed on the Mo content, which may be 0.000%. However, the Mo content is preferably 0.010% or more because Mo has the effect of improving hardenability and increasing the fractions of bainite and martensite.


Cr: 1.00% or Less

Cr has the effect of improving hardenability and increasing the fractions of bainite and martensite. When the Cr content exceeds 1.00%, the effect is saturated. No particular lower limit is placed on the Cr content, which may be 0.000%. However, the Cr content is preferably 0.01% or more because Cr has the effect of improving hardenability and increasing the fractions of bainite and martensite.


Cu: 1.00% or Less

Cu has the effect of increasing strength by the formation of a solute. When the Cu content exceeds 1.00%, intergranular cracking tends to be generated. No particular lower limit is placed on the Cu content, which may be 0.000%. However, the Cu content is preferably 0.01% or more because Cu has the effect of increasing strength by the formation of a solute.


Ni: 0.50% or Less

Ni has the effect of improving hardenability. However, when the Ni content exceeds 0.50%, the effect is saturated. No particular lower limit is placed on the Ni content, which may be 0.000%. However, the Ni content is preferably 0.01% or more because Ni has the effect of improving hardenability.


Sb: 0.200% or Less

Sb has the effect of suppressing surface oxidation, nitriding, and decarburization of steel sheets. However, when the Sb content exceeds 0.200%, the effect is saturated. No particular lower limit is placed on the Sb content, which may be 0.000%. However, the Sb content is preferably 0.001% or more because Sb has the effect of suppressing surface oxidation, nitriding, and decarburization of steel sheets.


Sn: 0.200% or Less

Sn, like Sb, has the effect of suppressing surface oxidation, nitriding, and decarburization of steel sheets. When the Sn content exceeds 0.200%, the effect is saturated. No particular lower limit is placed on the Sn content, which may be 0.000%. However, the Sn content is preferably 0.001% or more because Sn has the effect of suppressing surface oxidation, nitriding, and decarburization of steel sheets.


Ta: 0.200% or Less

Ta has the effect of forming fine carbides and increasing strength. When the Ta content exceeds 0.200%, coarse Ta carbides precipitate, and toughness is reduced. No particular lower limit is placed on the Ta content, which may be 0.000%. However, the Ta content is preferably 0.001% or more because Ta has the effect of forming fine carbides and increasing strength.


W: 0.400% or Less

W has the effect of forming fine carbides and increasing strength. When the W content exceeds 0.400%, coarse W carbides precipitate, and toughness is reduced. No particular lower limit is placed on the W content, which may be 0.000%. However, the W content is preferably 0.001% or more because W has the effect of forming fine carbides and increasing strength.


Zr: 0.0200% or Less

Zr has the effect of spheronizing the shape of inclusions, suppressing stress concentration, and improving toughness. When the Zr content exceeds 0.0200%, a large amount of inclusions are formed, and toughness is reduced. No particular lower limit is placed on the Zr content, which may be 0.000%. However, the Zr content is preferably 0.0001% or more because Zr has the effect of spheronizing the shape of inclusions, suppressing stress concentration, and improving toughness.


Ca: 0.0200% or Less

Ca can be used as a deoxidizing material. When the Ca content exceeds 0.0200%, a large amount of Ca-based inclusions are formed, and toughness is reduced. No particular lower limit is placed on the Ca content, which may be 0.000%. However, the Ca content is preferably 0.0001% or more because Ca can be used as a deoxidizing material.


Mg: 0.0200% or Less

Mg can be used as a deoxidizing material. When the Mg content exceeds 0.0200%, a large amount of Mg-based inclusions are formed, and toughness is reduced. No particular lower limit is placed on the Mg content, which may be 0.000%. However, the Mg content is preferably 0.0001% or more because Mg can be used as a deoxidizing material.


Co: 0.020% or Less

Co has the effect of increasing strength by solid solution strengthening. When the Co content exceeds 0.020%, the effect is saturated. No particular lower limit is placed on the Co content, which may be 0.000%. However, the Co content is preferably 0.001% or more because Co has the effect of increasing strength by solid solution strengthening.


REM: 0.0200% or Less

REM has the effect of spheronizing the shape of inclusions, suppressing stress concentration, and improving toughness. When the REM content exceeds 0.0200%, a large amount of inclusions are formed, and toughness is reduced. No particular lower limit is placed on the REM content, which may be 0.000%. However, the REM content is preferably 0.0001% or more because REM has the effect of spheronizing the shape of inclusions, suppressing stress concentration, and improving toughness.


Te: 0.020% or Less

Te has the effect of spheronizing the shape of inclusions, suppressing stress concentration, and improving toughness. When the Te content exceeds 0.020%, a large amount of inclusions are formed, and toughness is reduced. No particular lower limit is placed on the Te content, which may be 0.000%. However, the Te content is preferably 0.001% or more because Te has the effect of spheronizing the shape of inclusions, suppressing stress concentration, and improving toughness.


Hf: 0.10% or Less

Hf has the effect of spheronizing the shape of inclusions, suppressing stress concentration, and improving toughness. When the Hf content exceeds 0.10%, a large amount of inclusions are formed, and toughness is reduced. No particular lower limit is placed on the Hf content, which may be 0.000%. However, the Hf content is preferably 0.01% or more because Hf has the effect of spheronizing the shape of inclusions, suppressing stress concentration, and improving toughness.


Bi: 0.200% or Less

Bi has the effect of reducing segregation and improving bendability. When the Bi content exceeds 0.200%, a large amount of inclusions are formed, and bendability is reduced. No particular lower limit is placed on the Bi content, which may be 0.000%. However, the Bi content is preferably 0.001% or more because Bi has the effect of reducing segregation and improving bendability.


The balance other than the above-described components is Fe and inevitable impurities. The effect of this disclosure is not impaired when each of the contents of the above optional components is less than the lower limit. Thus, these optional components are treated as inevitable impurities when they are contained with a content that is less than the lower limit.


[Steel Microstructure]

Next, a steel microstructure of the high strength steel sheet will be described.


Martensite and Bainite: Total Area Ratio of 95% or More

Both martensite and bainite are hard phases and are necessary to achieve a TS of 1180 MPa or higher. Therefore, the total area ratio of martensite and bainite is 95% or more. The total area ratio of martensite and bainite is preferably 96% or more. No particular upper limit is placed on the total area ratio of martensite and bainite, which may be 100%.


The steel microstructure may contain residual microstructures other than martensite and bainite. The residual microstructures include ferrite, residual austenite, and cementite. The residual microstructures are 5% or less of the total area ratio.


The area ratio of each microstructure is measured as follows. The area ratio of residual austenite is obtained by chemically polishing the rolled surface of a test specimen taken from each steel sheet up to ¼t of the sheet thickness, measuring the X-ray diffraction intensity and diffraction peak positions of the polished surface using an X-ray diffraction (XRD) device, calculating the volume fraction, and considering the volume fraction as the area ratio of residual austenite. Next, a cross section of each steel sheet taken in the sheet thickness direction parallel to the rolling direction is polished and then etched with 3% nital, and the ¼t position of the sheet thickness is used as the observation plane. SEM images in three fields of view are taken of the observation plane at a magnification of 2000×. The total area ratio of martensite, bainite, and residual austenite and the area ratio of microstructures (ferrite and cementite) other than martensite, bainite, and residual austenite are determined by image analysis of the obtained SEM images. The area ratio of martensite and bainite is determined by subtracting the area ratio of residual austenite obtained by XRD from the area ratio of martensite, bainite, and residual austenite obtained by image analysis. The average value of the three fields of view is taken as the area ratio of the microstructure.


Average Grain Size of Prior Austenite Grains: 10 μm or Less

Toughness and bendability can be improved by refining crystal grains and complicating a crack propagation path. Further refining crystal grains and strengthening has the effect of increasing yield stress. To obtain these effects, the average grain size of prior austenite grains needs to be 10 μm or less. The average grain size of prior austenite grains is preferably 9 μm or less. No particular lower limit is placed on the average grain size of prior austenite grains. However, from the viewpoint of production technology, the average grain size of prior austenite grains is preferably 1 μm or more.


The average grain size of prior austenite grains is measured as follows. A cross section of each steel sheet taken in the sheet thickness direction parallel to the rolling direction is polished and then etched with picral, and three-fields-of-view SEM images are taken of the microstructure at the ¼t position of the sheet thickness with a magnification of 2000× in three fields of view. The grain size of each prior austenite grain is determined from the obtained microstructure image by image analysis, and the average value of the three fields of view is considered as the average grain size of prior austenite grains.


B Concentration at Prior Austenite Grain Boundary: 0.10% or More in Mass %

B can strengthen the grain boundary by segregating at the prior austenite grain boundary and improve toughness and bendability. This effect can be achieved when the B concentration at the prior austenite grain boundary is 0.10% or more in mass %. The B concentration at the prior austenite grain boundary is preferably 0.15% or more, and more preferably 0.20% or more in mass %. No upper limit is placed on the B concentration at the prior austenite grain boundary. However, the B concentration at the prior austenite grain boundary is preferably less than 20% to suitably prevent precipitation of hard carbon borides on the grain boundary and to further improve toughness.


The B concentration at the prior austenite grain boundary is measured as follows. A needle sample is prepared from the region containing the prior austenite grain boundary by the SEM-Focused Ion Beam (FIB) method. The obtained needle sample is subjected to 3DAP analysis using a 3Dimensional Atom Probe (3DAP) instrument (LEAP 4000X Si, made by AMETEK). The measurement is performed in laser mode. The B concentration at the prior austenite grain boundary is determined from the number of B ions and the number of other ions, which are detected from the prior austenite grain boundary.


C-Concentrated Region

Bendability and yield ratio can be improved by strengthening the martensitic grain boundary and the matrix phases sandwiching the martensitic grain boundary by C concentration. In this specification, “martensitic grain boundary” includes all of the prior austenite grain boundary, the block grain boundary, and the packet grain boundary that exist in martensite and bainite. FIG. 1A and FIG. 1B each illustrate an example of the C-concentrated region. FIG. 1A illustrates an observation result of a C-concentrated region that exists in the block grain boundary and the packet grain boundary. FIG. 1B illustrate an observation result of a C-concentrated region that exists in the prior austenite grain boundary. In FIG. 1A and FIG. 1B, the drawing on the left is an example of the observation result using a scanning transmission electron microscope (STEM), indicating the presence of a martensitic grain boundary in the center of the drawing. The drawing on the right is an example of the observation result of the C concentration amount using the STEM. From these drawings, it can be seen that there is a C-concentrated region along the martensitic grain boundary and across the base metals sandwiching the martensitic grain boundary.


C Concentration in C-Concentrated Region: 4.0 Times or More than C Content in Steel


Sufficient grain boundary strength can be achieved when C is concentrated to 4.0 times or more than the C content in the steel, in the C-concentrated region. That is, the C concentration in the C-concentrated region satisfies the following formula (2).






C concentration in C-concentrated region(mass %)/C content in steel(mass %)≥4.0  (2)


The C concentration in the C-concentrated region is preferably 4.5 times or more than the C content in the steel. No particular upper limit is placed on the C concentration in the C-concentrated region. However, the C concentration is preferably 6% or less to suitably prevent cementite precipitation and suitably prevent decrease in solute C concentration.


C-Concentrated Region: Concentration Width of 3 nm or More and 100 Nm or Less in Direction Perpendicular to Martensitic Grain Boundary

As illustrated in FIG. 1A and FIG. 1B, bendability and yield ratio can be improved by strengthening not only the martensitic grain boundary but also the matrix phases sandwiching the martensite grain boundary by C concentration. Therefore, the C-concentrated region is formed in a direction perpendicular to the martensitic grain boundary with a concentration width of 3 nm or more and 100 nm or less. When the concentration width of the C-concentrated region is less than 3 nm, the above effect is small. On the other hand, when the width of the C-concentrated region exceeds 100 nm, C cannot be sufficiently concentrated at the grain boundary and near the grain boundary. The width of the C-concentrated region is preferably 3.5 nm or more. The width of the C-concentrated region is preferably 80 nm or less.


C-Concentrated Region: Length of 100 nm or More in Direction Parallel to Martensitic Grain Boundary

To achieve excellent bendability and yield ratio, it is important to strengthen the martensitic grain boundary into a network by C segregation. Therefore, the C-concentrated region is formed with a length of 100 nm or more in a direction parallel to the martensitic grain boundary. When the length of the C-concentrated region is less than 100 nm, fracture and yielding occur from breaks in the C-concentrated region. The C-concentrated region preferably exists with a length of 120 nm or more in the direction parallel to the martensitic grain boundary. No upper limit is placed on the length of the C-concentrated region along the martensitic grain boundary. The C-concentrated region may exist so as to cover the entire length of the martensitic grain boundary.


The C concentration, concentration width, and length of the C-concentrated region are measured as follows. A thin film sample is prepared from the region including the martensite grain boundary by the SEM-FIB method and the area analysis of C is performed by STEM and energy dispersive X-ray spectroscopy (EDS). An analytical transmission electron microscope Talos F200X (made by FEI) is used for the analysis. The thin film sample is tilted so that the martensitic grain boundary is parallel to the electron beam, and the area analysis in a region of 200 nm×500 nm is performed. The analysis length in the direction parallel to the martensitic grain boundary (direction along the martensitic grain boundary) is 500 nm. The area analysis data is integrated in the direction parallel to the martensitic grain boundary to obtain a line profile with a length of 200 nm in the direction perpendicular to the martensitic grain boundary. In the line profile of C concentration, the half value of the maximum value of the line profile is determined, and the width that is equal to or more than the half value on the line profile is considered as the concentration width of the C-concentrated region. The C concentration in the C-concentrated region is determined by quantitative analysis of EDS for the concentration width. The length of the C-concentrated region is measured in the direction parallel to the martensitic grain boundary in the area analysis of C. The obtained length is considered as the length of the C-concentrated region along the martensitic grain boundary.


According to this disclosure, it is possible to provide a high strength steel sheet with a tensile strength of 1180 MPa or higher. The tensile strength of the high strength steel sheet is preferably 1250 MPa or higher.


The above-described high strength steel sheet may have a coated or plated layer on at least one surface. One of a hot-dip galvanized layer, a galvannealed layer, and an electrogalvanized layer is preferred as the coated or plated layer. No particular limitation is placed on the composition of the coated or plated layer. Any known composition can be used.


No particular limitation is placed on the composition of the hot-dip galvanized layer. A common composition may be used. In an example, the coated or plated layer contains: Fe: 20 mass % or less; and Al: 0.001 mass % or more and 1.0 mass % or less, and further contains one or two or more selected from the group consisting of Pb, Sb, Si, Sn, Mg, Mn, Ni, Cr, Co, Ca, Cu, Li, Ti, Be, Bi, and REM by the total content thereof in the range of 0 mass % or more and 3.5 mass % or less, with the balance being Zn and inevitable impurities. When the coated or plated layer is a hot-dip galvanized layer, in an example, the Fe content in the coated or plated layer is less than 7 mass %. When the coated or plated layer is a galvannealed layer, in an example, the Fe content in the coated or plated layer is 7 mass % or more and 15 mass % or less. More preferably, the Fe content in the coated or plated layer is 8 mass % or more, and the Fe content in the coated or plated layer is 13 mass % or less.


No particular limitation is placed on the coating weight. However, the coating weight per one surface of the high strength steel sheet is preferably 20 g/m2 or more, and the coating weight per one surface of the high strength steel sheet is preferably 80 g/m2 or less. In an example, the coated or plated layer is formed on the front and back surfaces of the high strength steel sheet.


Next, a method of producing a high strength steel sheet will be described.


First, a steel slab having the above-described chemical composition is produced. Steel materials are first smelted to produce molten steel having the above-described chemical composition. No particular limitation is placed on the smelting method. Any of known smelting methods, such as converter smelting and electric furnace smelting, can be applied. The resulting molten steel is solidified to produce a steel slab (slab). No particular limitation is placed on the method of producing a steel slab from molten steel. Continuous casting, ingot casting, thin slab casting, or other methods can be used. The steel slab may be cooled once and then heated again before hot rolling, or a casted steel slab may be continuously hot rolled without cooling it to room temperature. In consideration of rolling load and scale generation, the slab heating temperature is preferably 1100° C. or higher, and the slab heating temperature is preferably 1300° C. or lower. No particular limitation is placed on the slab heating method. For example, the slab can be heated in a heating furnace in accordance with a conventional method.


[Hot Rolling]

Next, the heated steel slab is hot rolled to form a hot-rolled sheet. No particular limitation is placed on the hot rolling. Hot rolling may be performed in accordance with a conventional method. No particular limitation is placed on the cooling after hot rolling. The hot-rolled sheet is cooled to a coiling temperature. The hot-rolled sheet is then coiled in a coil form. The coiling temperature is preferably 400° C. or higher. This is because coiling is easier without increasing the strength of the hot-rolled sheet when the coiling temperature is 400° C. or higher. The coiling temperature is more preferably 550° C. or higher. The coiling temperature is preferably 750° C. or lower to suitably prevent generation of thick scale and to further improve yield. Before pickling, the hot-rolled sheet may be subjected to heat treatment to be softened.


[Pickling]

Optionally, scale is removed from the hot-rolled sheet that has been coiled in a coil form. No particular limitation is placed on the method of removing scale. However, pickling is preferably performed while rewinding the hot-rolled coil to completely remove scale. No particular limitation is placed on the pickling method. Pickling may be performed in accordance with a conventional method.


[Cold Rolling]

The hot-rolled sheet, which has been optionally descaled, is cleaned as appropriate, and then cold-rolled to form a cold-rolled sheet. No particular limitation is placed on the method of cold rolling. Cold rolling may be performed in accordance with a conventional method.


[Annealing]

Next, an annealing process is performed, in which the cold-rolled sheet is heated to a first heating temperature of 850° C. or higher and 920° C. or lower and held for 10 seconds or longer, then the temperature is raised to a second heating temperature of 1000° C. or higher and 1200° C. or lower at an average heating rate of 50° C./s or more, and the sheet is cooled to 500° C. or lower at a cooling rate of 50° C./s or more within 5 seconds after reaching the second heating temperature.


First Heating Temperature of 850° C. or Higher and 920° C. or Lower

The cold-rolled sheet is then heated to the first heating temperature of 850° C. or higher and 920° C. or lower and held for 10 seconds or longer. To obtain a martensite and bainite-dominated microstructure, annealing is performed at the first heating temperature in the austenite single phase region. When the first heating temperature is less than 850° C., ferrite is generated, and strength is reduced. On the other hand, when the first heating temperature exceeds 920° C., the austenite grain size exceeds 10 μm, and bendability, toughness, and yield ratio are reduced because the subsequent processes cannot reduce the grain size The first heating temperature is preferably 860° C. or higher. The first heating temperature is preferably 900° C. or lower.


Holding Time at First Heating Temperature: 10 Seconds or Longer

The holding time at the first heating temperature is 10 seconds or longer. By holding the sheet at the first heating temperature for 10 seconds or longer, the growth of austenite grain size is balanced by pinning by Nb carbides or growth inhabitation by solute Nb. When the holding time is less than 10 seconds, the austenite grains are in the process of growing, and the effect of pinning by Nb carbides or growth inhabitation by solute Nb does not occur during the subsequent rapid heating, and the prior austenite grain size exceeds 10 μm. No particular upper limit is placed on the holding time at the first heating temperature. However, from the viewpoint of productivity, the holding time at the first heating temperature is preferably 60 seconds or shorter. The holding time at the first heating temperature is preferably 20 seconds or longer.


Second Heating Temperature of 1000° C. or Higher and 1200° C. or Lower

After holding the sheet at the first heating temperature, the sheet is annealed at high temperature while maintaining the austenite grain boundary at 10 μm or less to cause a sufficient amount of B to segregate at the grain boundary. When the second heating temperature is less than 1000° C., B diffusion is slow, and grain boundary segregation is insufficient. When the second heating temperature exceeds 1200° C., austenite grain growth is rapid, and the austenite grain size exceeds 10 μm. The second heating temperature is preferably 1020° C. or higher. The second heating temperature is preferably 1150° C. or lower.


Average Heating Rate: 50° C./s or More

An average heating rate from the first heating temperature to the second heating temperature is 50° C./s or more. When the average heating rate from the first heating temperature to the second heating temperature is less than 50° C./s, the austenite grain size grows to more than 10 μm. No particular upper limit is placed on the average heating rate from the first heating temperature to the second heating temperature. However, the average heating rate is preferably 120° C./s or less because excessive rapid heating is difficult to control. The average heating rate from the first heating temperature to the second heating temperature is preferably 80° C./s or more.


Cooling at Average Cooling Rate of 50° C./s or More to 500° C. or Lower within 5 Seconds after Reaching Second Heating Temperature


After reaching the second heating temperature, rapid cooling is started within 5 seconds after reaching the second heating temperature without holding the sheet at the second heating temperature, and the rapid cooling is performed at an average cooling rate of 50° C./s or more to 500° C. or lower. This can produce a steel microstructure with an austenite grain size of 10 μm or less and B segregated at the grain boundary by 0.1% or more. Cooling is started immediately after the second heating temperature is reached because grain growth starts quickly after holding the sheet at the second heating temperature.


Average Cooling Rate: 50° C./s or More

In the cooling after reaching the second heating temperature, an average cooling rate from the second heating temperature to 500° C. or lower is 50° C./s or more. When the average cooling rate from the second heating temperature to 500° C. or lower is less than 50° C./s, grain growth occurs during cooling. No particular upper limit is placed on the average cooling rate from the second heating temperature to 500° C. or lower. However, the average cooling rate is preferably 120° C./s or less to facilitate control. The average cooling rate from the second heating temperature to 500° C. or lower is preferably 80° C./s or more.


Cooling Stop Temperature: 500° C. or Lower

To inhibit ferrite transformation, rapid cooling is performed to a cooling stop temperature of 500° C. or lower. The cooling stop temperature is preferably 450° C. or lower. No particular lower limit is placed on the cooling stop temperature. However, the cooling stop temperature is preferably 100° C. or higher.


After the above-described annealing process and before a reheating process, a coating or plating process may be performed, in which at least one surface of the high strength steel sheet is subjected to coating or plating treatment to obtain a high strength coated or plated steel sheet. After the coating or plating process, the high strength coated or plated steel sheet may be subjected to heat treatment to alloy the coated or plated layer of the high strength coated or plated steel sheet, resulting in a galvannealed steel sheet.


After Annealing Process, Rolling Process in which Rolling with an Elongation Rate of 0.5% or More is Performed


After the above-described annealing process, a rolling process is performed, in which the cold-rolled sheet is rolled at an elongation rate of 0.5% or more to obtain a second cold-rolled sheet. The cold-rolled sheet obtained in the preceding process contains many mobile dislocations. In this rolling process, the mobile dislocations accumulate at the grain boundary and become entangled to form immobile dislocations. When the elongation rate is less than 0.5%, the effect is small. The elongation rate in the rolling process is preferably 0.6% or more. No particular upper limit is placed on the elongation rate in the rolling process. However, the elongation rate is preferably 2% or less, for example, to reduce the load on the equipment.


After Rolling Process, Reheating Process in which Second Cold-Rolled Sheet is Held at Reheating Temperature of 70° C. or Higher and 200° C. or Lower for 600 Seconds or Longer


After the above-described rolling process, the second cold-rolled sheet is tempered at low temperature in order to segregate C on the dislocations accumulated near the grain boundary or to generate clusters. When the reheating temperature is less than 70° C., C diffusion is slow, and C is not concentrated near the grain boundary to a sufficient amount. On the other hand, when the reheating temperature exceeds 200° C., tempering excessively proceeds, and cementite precipitates. The cementite precipitated at the grain boundary is likely to be a fracture origin, and the C concentration of the matrix phases around the cementite is reduced, resulting in reduced bendability and toughness. The reheating temperature is preferably 90° C. or higher. The reheating temperature is preferably 190° C. or lower.


Holding Time at Reheating Temperature: 600 Seconds or Longer

When the holding time at the reheating temperature is less than 600 seconds, C diffusion is slow, and a sufficient amount of C concentration is not obtained. No particular upper limit is placed on the holding time at the reheating temperature. However, the holding time is preferably 43200 seconds (0.5 days) or shorter to prevent cementite precipitation. The holding time at the reheating temperature is preferably 800 seconds or longer.


In the case of reheating without the rolling process, C segregates at the grain boundary, and toughness is improved. However, the concentration width is narrow and regions except for the grain boundary is not strengthened, resulting in poor bendability. In addition, dislocations remain mobile dislocations, resulting in poor YR.


Production conditions other than those described above can be determined in accordance with conventional methods.


[Member]

It is possible to provide a member formed using the above-described high strength steel sheet or high strength coated or plated steel sheet, for at least a portion thereof. The above-described high strength steel sheet or high strength coated or plated steel sheet can be formed into a desired shape by press working, in an example, to form an automotive part. The automotive part may contain steel sheets other than the high strength steel sheet or high strength coated or plated steel sheet according to this embodiment, as its materials. According to this embodiment, it is possible to provide a high strength steel sheet with a TS of 1180 MPa or higher, bendability, toughness, and a high yield ratio. Therefore, the high strength steel sheet or high strength coated or plated steel sheet according to this embodiment is suitable for automotive parts that contribute to weight reduction of the automotive body. This high strength steel sheet or high strength coated or plated steel sheet can be suitably used for automotive parts, in particular, members used as skeletal structural parts or reinforcement parts in general.


Examples

Steel having the chemical compositions presented in Table 1, with the balance being Fe and inevitable impurities, was smelted in a converter furnace to form steel slabs. The resulting slabs were reheated, hot rolled, and then coiled to obtain hot-rolled coils. The hot-rolled coils were then subjected to pickling treatment while being rewound, and then cold rolled. The thickness of the hot-rolled sheets was 3.0 mm, and the thickness of the cold-rolled sheets was 1.2 mm. Annealing was performed in a continuous hot-dip galvanizing line under the conditions presented in Table 2 to obtain cold-rolled steel sheets, hot-dip galvanized steel sheets (GI), and galvannealed steel sheets (GA). The hot-dip galvanized steel sheets were immersed in a plating bath at 460° C. to achieve a coating weight of 35 g/m2 per surface. The galvannealed steel sheets were produced by adjusting the coating weight to 45 g/m2 per surface, followed by alloying treatment at 520° C. for 40 seconds. The resulting steel sheets were subjected to rolling and reheat treatment under the conditions presented in Table 2.


For each resulting steel sheet, the total area ratio of martensite and bainite, the prior austenite grain size, the B concentration at the prior austenite grain boundary, the C concentration in the C-concentrated region at the martensitic grain boundary (mass %)/the C content in the steel (mass %), the concentration width of the C-concentrated region, and the length along the martensite grain boundary in the C-concentrated region were evaluated according to the above-described methods. The tensile strength, yield ratio, toughness, and bendability were also evaluated according to the methods described below. The results are presented in Table 3.


[Tensile Test]


The resulting steel sheets were subjected to a tensile test in accordance with JIS Z 2241. JIS No. 5 tensile test specimens were taken having a longitudinal direction perpendicular to the rolling direction, and the tensile test was conducted to measure the tensile strength (TS) and yield stress (YS). The tensile strength was considered good when the tensile strength TS was 1180 MPa or higher. A ratio of yield stress to tensile strength, YR=YS/TS, of 0.80 or higher indicates a high yield ratio.


[Charpy Test]


Charpy impact test was conducted in accordance with JIS Z 2242. From each resulting steel sheet, a test specimen with a width of 10 mm, a length of 55 mm, and a 900 V-notch with a notch depth of 2 mm at the center of the length was taken such that the direction perpendicular to the rolling direction of the steel sheet was a V-notching direction. The Charpy impact test was then conducted in a test temperature range of −120° C. to +120° C. The transition curve was determined from the obtained percent brittle fracture, and the temperature at which the percent brittle fracture reaches 50% was determined as a brittle-ductile transition temperature. The toughness was considered good when the brittle-ductile transition temperature obtained from the Charpy test was −40° C. or lower. In the table, brittle-ductile transition temperatures of −40° C. or lower were indicated as “Excellent” for toughness, and brittle-ductile transition temperatures exceeding −40° C. were indicated as “Poor” for toughness.


[Bend Test]

Bend test was conducted in accordance with JIS Z 2248. From each resulting steel sheet, a strip test specimen with a width of 30 mm and a length of 100 mm was taken such that the direction parallel to the rolling direction of the steel sheet was the axial direction in the bend test. Then, 900 V-bend test was conducted under a set of conditions including a pushing load of 100 kN and a pressing holding time of 5 seconds. The bendability was evaluated by the pass rate in the bend test. The bend test for five samples was conducted at the maximum R where R/t, the value obtained by dividing the bend radius (R) by the sheet thickness (t), is 5 or less (e.g., when the sheet thickness is 1.2 mm, the bend radius is 7.0 mm). Next, the presence of cracks at the ridge of the tip of the bending test specimen was evaluated. The bendability was considered good only when none of the five samples cracked, i.e., when the pass rate was 100%. In the table, only cases when the pass rate was 100% are indicated as “Excellent” for bendability and other cases are indicated as “Poor” for bendability. The presence of cracks was evaluated by measuring the ridge of the tip of the bending test specimen using a digital microscope (RH-2000: made by Hirox Co., Ltd.) with a magnification of 40×.











TABLE 1







Steel
Chemical composition (mass %)
([% N]/14)/



















sample ID
C
Si
Mn
P
S
Al
N
Ti
Nb
B
Other
([% Ti]/47.9)





A
0.15
1.10
3.2
0.011
0.0010
0.040
0.0041
0.018
0.011
0.0012

0.78


B

0.09

0.95
2.9
0.015
0.0018
0.036
0.0035
0.021
0.015
0.0018

0.57


C

0.34

1.03
3.3
0.021
0.0020
0.042
0.0052
0.020
0.022
0.0018

0.89


D
0.19
0.65
3.5
0.018
0.0012
0.038
0.0038
0.018

0.001

0.0016

0.72


E
0.22
0.66
3.4
0.022
0.0016
0.040
0.0036
0.022

0.082

0.0017

0.56


F
0.24
0.82
3.0
0.016
0.0009
0.042
0.0044
0.021
0.035

0.0001


0.72


G
0.20
1.10
2.9
0.012
0.0014
0.039
0.0033
0.017
0.042

0.0084


0.66


H
0.19
0.78
3.4
0.016
0.0010
0.036
0.0058
0.015
0.027
0.0022


1.32



I
0.16
0.85
3.2
0.011
0.0012
0.037
0.0042
0.022
0.031
0.0020
Cr 0.21, Mo 0.272
0.65


J
0.12
1.01
3.7
0.012
0.0009
0.039
0.0033
0.024
0.005
0.0021
V 0.080
0.47


K
0.22
0.81
2.8
0.018
0.0021
0.045
0.0061
0.032
0.018
0.0016
Cu 0.11, Ca 0.0005
0.65


L
0.27
0.96
2.7
0.010
0.0008
0.029
0.0032
0.015
0.032
0.0020
Ni 0.12, Ta 0.007
0.73


M
0.18
0.99
2.9
0.008
0.0015
0.039
0.0028
0.020
0.023
0.0015
Sb 0.009, Mg 0.0010
0.48


N
0.18
0.76
3.1
0.011
0.0009
0.039
0.0040
0.021
0.011
0.0022
Sn 0.008, Co 0.008
0.65


O
0.25
0.92
2.9
0.012
0.0014
0.044
0.0033
0.018
0.041
0.0021
REM 0.0022
0.63


P
0.17
0.91
3.1
0.013
0.0011
0.038
0.0028
0.021
0.021
0.0017
W 0.122, Zr 0.0018
0.46


Q
0.18
0.99
3.2
0.012
0.0013
0.035
0.0036
0.020
0.024
0.0022

0.62


R
0.19
0.85
2.9
0.011
0.0012
0.040
0.0038
0.018
0.016
0.0019
Te 0.005, Hf 0.02, Bi 0.002
0.72





Underlines indicate outside the appropriate range of this disclosure.
























TABLE 2










Average heating
Average cooling









First

Second
rate from first
rate from second




heating
Hold-
heating
heating temperature
heating temperature

Elon-
Reheating
Hold-



Steel
temper-
ing
temper-
to second heating
to 500° C.
Coating
gation
temper-
ing



sample
ature
time
ature
temperature
or lower
or
rate
ature
time


No.
ID
(° C.)
(s)
(° C.)
(° C./s)
(° C./s)
plating
(%)
(° C.)
(s)
Remarks


























1
A
870
40
1110
80
80
Without
1.2
170
1200
Example


2
A
860
30
1100
60
60
GI
1.4
180
 800
Example


3
A
900
30
1140
80
80
GA
1.0
 90
10800 
Example


4
A

830

50
1150
80
80
GI
1.2
120
3600
Comparative Example


5
A
880
5
1120
80
80
Without
1.2
180
1500
Comparative Example


6
A
900
20
980
80
80
Without
1.0
150
2400
Comparative Example


7
A
890
40

1210

80
80
GA
0.8
140
3600
Comparative Example


8
A
860
40
1100

40

80
Without
0.6
100
7200
Comparative Example


9
A
870
30
1190
80

40

Without
0.8
150
2400
Comparative Example


10

B

860
30
1100
80
80
GA
0.8
160
1200
Comparative Example


11

C

880
40
1120
80
80
GI
0.6
120
3000
Comparative Example


12

D

900
40
1060
80
80
GA
1.2
170
1800
Comparative Example


13

E

910
50
1070
80
80
GA
0.6
100
10800 
Comparative Example


14

F

900
30
1140
80
80
GA
1.2
150
2400
Comparative Example


15

G

890
40
1130
80
80
GA
0.6
120
1800
Comparative Example


16

H

890
40
1050
80
80
GA
0.8
140
2400
Comparative Example


17
I
860
50
1180
80
80
GA
1.2
180
 700
Example


18
J
910
50
1150
80
80
GI
1.2
 80
10800 
Example


19
K
890
30
1130
80
80
GI
0.6
130
7200
Example


20
L
870
50
1030
80
80
Without
0.6
120
7200
Example


21
M
890
40
1130
80
80
GA
0.8
150
3600
Example


22
N
900
50
1140
80
80
GA
0.8
160
1500
Example


23
O
880
30
1040
80
80
GA
0.6
120
7200
Example


24
P
870
40
1110
80
80
GA
1.0
150
3600
Example


25
Q
900
40
1060
80
80
GA
1.0
140
3600
Example


26
Q
880
50
1120
80
80
GA
0.8
60
7200
Comparative Example


27
Q
910
40
1150
80
80
GA
0.8
150
500
Comparative Example


28
Q
900
40
1110
80
80
GA
1.0

230

1800
Comparative Example


29
Q
880
30
1040
80
80
GA

0.2

180
1200
Comparative Example


30
Q
900
40
1060
80
80
GA

None

140
3600
Comparative Example


31
R
890
40
1120
80
80
Without
0.8
160
 900
Example





Underlines indicate outside the appropriate range of this disclosure.





















TABLE 3









Total area

Prior
B concentration
Concentration
C concentration
Length




ratio of

austenite
at prior
width of C-
in C-concentrated
of C-



Steel
martensite

grain
austenite
concentrated
region (mass %)/
concentrated



sample
and bainite
Residual
size
grain boundary
region
C content in steel
region


No.
ID
(%)
microstructure
(μm)
(mass %)
(nm)
(mass %)
(nm)





1
A
99
Residual γ
6
0.25
15
5.2
320


2
A
99
Residual γ
5
0.31
22
4.8
220


3
A
99
Residual γ
6
0.22
 8
4.8
180


4
A

88

Ferrite
6
0.25
24
4.3
220


5
A
99
Residual γ

12

0.43
15
4.2
310


6
A
99
Residual γ
8

0.07

10
4.6
280


7
A
99
Residual γ

14

0.44
12
4.5
190


8
A
99
Residual γ

15

0.38
 8
4.2
260


9
A
99
Residual γ

12

0.42
22
4.8
170


10

B


87

Ferrite
7
0.32
14
5.2
140


11

C

99
Residual γ
8

0.06

28
4.1
200


12

D

99
Residual γ

18

0.37
17
4.1
180


13

E

99
Residual γ
5
0.28
16
4.9
230


14

F

99
Residual γ
6

0.00

10
4.4
220


15

G

99
Residual γ
7
0.52
13
4.8
130


16

H

99
Residual γ

12


0.04

14
4.7
180


17
I
99
Residual γ
6
0.26
11
5.1
250


18
J
99
Residual γ
7
0.33
 6
6.2
240


19
K
99
Residual γ
6
0.29
10
4.4
160


20
L
99
Residual γ
7
0.29
13
4.2
180


21
M
99
Residual γ
6
0.27
18
4.6
190


22
N
99
Residual γ
7
0.31
21
5.1
120


23
O
99
Residual γ
6
0.40
 5
4.2
200


24
P
99
Residual γ
7
0.35
12
4.9
240


25
Q
99
Residual γ
8
0.34
13
5.2
230


26
Q
99
Residual γ
7
0.33
2
4.9
120


27
Q
99
Residual γ
7
0.29
64

3.4

200


28
Q
99
Residual γ
7
0.31

130


1.8

220


29
Q
99
Residual γ
7
0.42
 4
4.1
70


30
Q
99
Residual γ
8
0.29
2

2.7

60


31
R
99
Residual γ
6
0.32
18
4.6
210
























Brittle-ductile










transition




TS
YS


temperature



No.
(MPa)
(MPa)
YR
Toughness
(° C.)
Bendability
Remarks







1
1283
1102
0.86
Excellent
−80
Excellent
Example



2
1318
1142
0.87
Excellent
−60
Excellent
Example



3
1291
1089
0.84
Excellent
−60
Excellent
Example



4
1052
793
0.75
Excellent
−80
Excellent
Comparative Example



5
1233
1022
0.83
Poor
−20
Poor
Comparative Example



6
1303
1084
0.83
Poor
0
Poor
Comparative Example



7
1228
984
0.80
Poor
−10
Poor
Comparative Example



8
1212
994
0.82
Poor
−20
Poor
Comparative Example



9
1233
1008
0.82
Poor
−30
Poor
Comparative Example



10
1030
721
0.70
Excellent
−60
Excellent
Comparative Example



11
1581
1320
0.83
Poor
0
Poor
Comparative Example



12
1333
1126
0.84
Poor
−20
Poor
Comparative Example



13
1509
1288
0.85
Poor
−20
Poor
Comparative Example



14
1521
1289
0.85
Poor
0
Poor
Comparative Example



15
1490
1225
0.82
Poor
0
Poor
Comparative Example



16
1455
1206
0.83
Poor
0
Poor
Comparative Example



17
1236
1061
0.86
Excellent
−60
Excellent
Example



18
1202
1011
0.84
Excellent
−70
Excellent
Example



19
1521
1276
0.84
Excellent
−50
Excellent
Example



20
1522
1264
0.83
Excellent
−50
Excellent
Example



21
1366
1118
0.82
Excellent
−80
Excellent
Example



22
1229
1020
0.83
Excellent
−80
Excellent
Example



23
1502
1263
0.84
Excellent
−50
Excellent
Example



24
1202
1021
0.85
Excellent
−80
Excellent
Example



25
1341
1130
0.84
Excellent
−60
Excellent
Example



26
1386
1029
0.74
Poor
0
Poor
Comparative Example



27
1404
1084
0.77
Poor
−20
Poor
Comparative Example



28
1306
975
0.75
Poor
0
Poor
Comparative Example



29
1442
1081
0.75
Excellent
−60
Poor
Comparative Example



30
1335
1021
0.76
Excellent
−50
Poor
Comparative Example



31
1290
1071
0.83
Excellent
−80
Poor
Example







Underlines indicate outside the appropriate range of this disclosure.






Table 3 presents that the examples each have a TS of 1180 MPa or higher, a yield ratio of 0.80 or higher, and excellent bendability and toughness. On the other hand, one or more of the TS, yield ratio, bendability, and toughness are poor in the comparative examples.

Claims
  • 1. A high strength steel sheet comprising a chemical composition containing, in mass %: C: 0.10% or more and 0.30% or less;Si: 0.20% or more and 1.20% or less;Mn: 2.5% or more and 4.0% or less;P: 0.050% or less;S: 0.020% or less;Al: 0.10% or less;N: 0.01% or less;Ti: 0.100% or less;Nb: 0.002% or more and 0.050% or less; andB: 0.0005% or more and 0.0050% or less,
  • 2. The high strength steel sheet according to claim 1, wherein the chemical composition further contains at least one element selected from, in mass %: V: 0.100% or less;Mo: 0.500% or less;Cr: 1.00% or less;Cu: 1.00% or less;Ni: 0.50% or less;Sb: 0.200% or less;Sn: 0.200% or less;Ta: 0.200% or less;W: 0.400% or less;Zr: 0.0200% or less;Ca: 0.0200% or less;Mg: 0.0200% or less;Co: 0.020% or less;REM: 0.0200% or less;Te: 0.020% or less;Hf: 0.10% or less; orBi: 0.200% or less.
  • 3. A high strength coated or plated steel sheet having a coated or plated layer on at least one surface of the high strength steel sheet according to claim 1.
  • 4. A method of producing a high strength steel sheet, comprising: hot rolling a steel slab having the chemical composition according to claim 1 to form a hot-rolled sheet;cold rolling the hot-rolled sheet to form a cold-rolled sheet;performing an annealing process in which the cold-rolled sheet is heated to a first heating temperature of 850° C. or higher and 920° C. or lower and held for 10 seconds or longer, the temperature is then raised to a second heating temperature of 1000° C. or higher and 1200° C. or lower at an average heating rate of 50° C./s or more, and the sheet is cooled to 500° C. or lower at an average cooling rate of 50° C./s or more within 5 seconds after reaching the second heating temperature,after the annealing process, performing a rolling process in which the cold-rolled sheet is rolled at an elongation rate of 0.5% or more to obtain a second cold-rolled sheet, andafter the rolling process, performing a reheating process in which the second cold-rolled sheet is held at a reheating temperature of 70° C. or higher and 200° C. or lower for 600 seconds or longer to obtain a high strength steel sheet.
  • 5. A method of producing a high strength coated or plated steel sheet, comprising a coating or plating process in which, after the annealing process according to claim 4 and before the reheating process, at least one surface of the high strength steel sheet is subjected to coating or plating treatment to obtain a high strength coated or plated steel sheet.
  • 6. A member formed using the high strength steel sheet according to claim 1 for at least a portion thereof.
  • 7. A member formed using the high strength coated or plated steel sheet according to claim 3 for at least a portion thereof.
  • 8. A high strength coated or plated steel sheet having a coated or plated layer on at least one surface of the high strength steel sheet according to claim 2.
  • 9. A method of producing a high strength steel sheet, comprising: hot rolling a steel slab having the chemical composition according to claim 2 to form a hot-rolled sheet;cold rolling the hot-rolled sheet to form a cold-rolled sheet;performing an annealing process in which the cold-rolled sheet is heated to a first heating temperature of 850° C. or higher and 920° C. or lower and held for 10 seconds or longer, the temperature is then raised to a second heating temperature of 1000° C. or higher and 1200° C. or lower at an average heating rate of 50° C./s or more, and the sheet is cooled to 500° C. or lower at an average cooling rate of 50° C./s or more within 5 seconds after reaching the second heating temperature,after the annealing process, performing a rolling process in which the cold-rolled sheet is rolled at an elongation rate of 0.5% or more to obtain a second cold-rolled sheet, andafter the rolling process, performing a reheating process in which the second cold-rolled sheet is held at a reheating temperature of 70° C. or higher and 200° C. or lower for 600 seconds or longer to obtain a high strength steel sheet.
  • 10. A method of producing a high strength coated or plated steel sheet, comprising a coating or plating process in which, after the annealing process according to claim 9 and before the reheating process, at least one surface of the high strength steel sheet is subjected to coating or plating treatment to obtain a high strength coated or plated steel sheet.
  • 11. A member formed using the high strength steel sheet according to claim 2 for at least a portion thereof.
  • 12. A member formed using the high strength coated or plated steel sheet according to claim 8 for at least a portion thereof.
Priority Claims (1)
Number Date Country Kind
2021-140360 Aug 2021 JP national
PCT Information
Filing Document Filing Date Country Kind
PCT/JP2022/024762 6/21/2022 WO