FIELD
[0001] The present invention relates to a steel sheet.
BACKGROUND
[0002] In recent years, to deal with environmental issues, lightening the weight of auto
parts has been desired for the purpose of reduction of emission of CO
2 gas and improvement of fuel efficiency. On the other hand, there have been increasing
social calls for improvement of collision safety. To achieve both lighter weight and
improved collision safety, increasing the strength of steel materials is an effective
means. However, usually, if increasing the strength of steel materials, the workability
falls, and therefore steel materials simultaneously improved in strength and workability
have been considered necessary.
[0003] In relation to improvement of strength and workability, for example, PTL 1 describes
a hot rolled steel sheet having a chemical composition containing, by mass%, C: 0.020
to 0.070%, Si: 0.10 to 1.70%, Mn: 0.60 to 2.50%, Al: 0.01 to 1.00%, Ti: 0.015 to 0.170%,
Nb: 0.005 to 0.050%, etc., limiting P: 0.05% or less, S: 0.010% or less, and N: 0.0060%
or less, and having a balance of Fe and impurities, having a structure containing
an area ratio of 5 to 60% of ferrite and 30 to 95% of bainite, in which structure,
a boundary with an orientation difference of 15° or more being deemed a grain boundary,
when defining a region surrounded by the grain boundaries and with a circle equivalent
diameter of 0.3 µm or more as a "crystal grain", having a ratio of crystal grains
with an orientation difference in the grains of 5 to 14° of an area% of 20 to 100%.
Further, PTL 1 teaches that by making the ratio of crystal grains with an orientation
difference in the grains of 5 to 14° an area ratio of 20% or more, it is possible
to maintain the desired steel sheet strength while improving the stretch flangeability
(hole expandability).
[0004] PTL 2 describes a high strength steel material with prior γ grains of a spherical
shape containing, by mass ratio, C: 0.06 to 0.19%, Si: 0.15 to 0.60%, Mn: 0.60 to
1.80%, Cr: 0.05 to 1.20%, and Mo: 0.05 to 1.00% and containing one or more of Nb:
0.005 to 0.10%, V: 0.005 to 0.10%, and Ti: 0.005 to 0.10%, which steel material containing
carbonitrides of Nb, Ti, or V with a particle size of 100 nm or less in a volume ratio
of 0.01 to 0.8%, having prior γ grains of a particle size no. 7 or more, and having
a martensite structure or a mixed structure of martensite and bainite in the prior
γ grains. Further, PTL 2 teaches that according to the above configuration, it becomes
possible to provide high strength steel material excellent in toughness, arrestability,
and weldability and having a large uniform elongation property of more than 10% and
a good mass producibility.
[0005] PTL 3 describes a high carbon steel sheet member containing C: 0.80 mass% to 1.10
mass%, Si: 0.05 mass% to 0.40 mass%, Mn: 0.05 mass% to 0.50 mass%, Cr: 0.01 mass%
to 0.35 mass%, P: 0.03 mass% or less, and S: 0.03 mass% or less and having a balance
of Fe and unavoidable impurities, in which high carbon steel sheet member, a circle
equivalent diameter of martensite blocks defined by an orientation difference of 15°
or more being 3.2 µm or less, carbides of a circle equivalent diameter of 0.2 µm or
more being present in 0.6 to 5.0 area%, an average particle size of the carbides being
0.3 µm or more and 2.0 µm or less, a carbon occupancy on the prior austenite grain
boundaries being 0.35% or less, and an average value of KAM measured by EBSD being
0.690 to 0.710. Further, PTL 3 teaches that according to this configuration, it is
possible to obtain a high carbon steel sheet member with high levels of both hardness
and hardness-toughness balance.
[CITATION LIST]
[PATENT LITERATURE]
SUMMARY
[TECHNICAL PROBLEM]
[0007] As explained above, it is known that along with higher strength, the workability
of a steel material falls and the hole expandability and other properties fall such
as described in PTL 1. If the hole expandability falls, for example, sometimes it
is not possible to work the steel into a desired shape in transmission parts of automobiles,
etc. For this reason, in the development of a high strength hot rolled steel sheet
and other high strength steel sheet, it is important to secure the properties corresponding
to the application to a certain extent or more while trying to raise the strength.
Further, a steel sheet for automobile use is usually worked into the shape of the
desired part by press-forming. Usually, press-forming is performed divided into several
steps, and therefore there are a relatively large number of locations for example
receiving primary deformation and accumulating strain inside the steel sheet and,
in that state, again receiving separate deformation (stretch flange deformation, etc.)
However, if strain is introduced into a steel sheet, work hardening occurs and the
strength becomes higher, and therefore the workability in the later steps generally
falls. For this reason, a steel sheet is being asked to exhibit high formability by
for example having excellent work hardening ability (performance of continuing to
become harder) even in a state where a certain degree of strain is introduced.
[0008] The present invention was made in consideration of this actual situation and has
as its object to provide, by a novel constitution, a steel sheet which, despite being
high strength, is improved in hole expandability and work hardening ability.
[SOLUTION TO PROBLEM]
[0009] The inventors engaged in studies focusing on the microstructure of a steel sheet,
in particular a hot rolled steel sheet, to achieve the above object. As a result,
the inventors discovered that by making the microstructure of a hot rolled steel sheet
having a predetermined chemical composition a structure mainly comprised of martensite,
it is possible to achieve higher strength and improved hole expandability and that
by limiting the mean particle size of prior austenite grains in the microstructure
to within a predetermined range while suitably controlling the ratio of crystal grains
having a predetermined grain orientation difference in the martensite structure, it
is possible to remarkably improve the work hardening ability, and thereby completed
the present invention.
[0010] The present invention able to achieve the above object is as follows:
- (1) A steel sheet
having a chemical composition comprising, by mass%,
C: 0.040 to 0.200%,
Si: 0.30 to 2.00%,
Mn: 1.00 to 4.00%,
sol. Al: 0.001 to 0.500%,
P: 0.100% or less,
S: 0.0300% or less,
N: 0.0070% or less,
O: 0.0100% or less,
Nb: 0.001 to 1.000%,
Ti: 0 to 0.200%,
V: 0 to 0.300%,
Cu: 0 to 0.40%,
Cr: 0 to 0.90%,
Mo: 0 to 0.12%,
Ni: 0 to 0.30%,
B: 0 to 0.0030%,
Ca: 0 to 0.0010%,
Mg: 0 to 0.0010%,
Bi: 0 to 0.010%,
Zr: 0 to 0.050%,
Co: 0 to 0.010%,
Zn: 0 to 0.010%,
W: 0 to 0.100%,
Sn: 0 to 0.040%,
As: 0 to 0.100%,
REM: 0 to 0.0100%, and
balance: Fe and impurities, and
a microstructure comprising, by area%,
martensite: 90.0% or more, and
retained austenite: 3.0% or less, wherein
a mean particle size of prior austenite grains is 30.0 µm or less, and
when defining a region surrounded by grain boundaries with an orientation difference
of 15° or more in the martensite as a "crystal grain", a ratio of crystal grains with
an orientation difference in the grains of 4° or more is, by area%, 45.0 to 70.0%.
- (2) The steel sheet according to the above (1), wherein the chemical composition comprises,
by mass%, at least one of
Ti: 0.001 to 0.200%,
V: 0.001 to 0.300%,
Cu: 0.001 to 0.40%,
Cr: 0.001 to 0.90%,
Mo: 0.001 to 0.12%,
Ni: 0.001 to 0.30%,
B: 0.0001 to 0.0030%,
Ca: 0.0001 to 0.0010%,
Mg: 0.0001 to 0.0010%,
Bi: 0.001 to 0.010%,
Zr: 0.001 to 0.050%,
Co: 0.001 to 0.010%,
Zn: 0.001 to 0.010%,
W: 0.001 to 0.100%,
Sn: 0.001 to 0.040%,
As: 0.001 to 0.100%, and
REM: 0.0001 to 0.0100%.
- (3) The steel sheet according to the above (1) or (2), wherein the microstructure
further comprises, by area%, at least one of
ferrite: 10.0% or less,
bainite: 10.0% or less, and
pearlite: 10.0% or less.
- (4) The steel sheet according to any one of the above (1) to (3), wherein a ratio
of prior austenite grains with an aspect ratio of 2.0 or less in all prior austenite
grains is, by area%, 90.0% or more.
- (5) The steel sheet according to any one of the above (1) to (4), wherein a sheet
thickness is 1.0 to 7.0 mm.
- (6) A part including the steel sheet according to any one of the above (1) to (5).
[ADVANTAGEOUS EFFECTS OF INVENTION]
[0011] According to the present invention, it is possible to provide a steel sheet, in particular
a hot rolled steel sheet, which, despite being high strength, is improved in hole
expandability and work hardening ability.
DESCRIPTION OF EMBODIMENTS
<Steel Sheet>
[0012] The steel sheet according to an embodiment of the present invention, in particular
the hot rolled steel sheet, has a chemical composition comprising, by mass%,
C: 0.040 to 0.200%,
Si: 0.30 to 2.00%,
Mn: 1.00 to 4.00%,
sol. Al: 0.001 to 0.500%,
P: 0.100% or less,
S: 0.0300% or less,
N: 0.0070% or less,
O: 0.0100% or less,
Nb: 0.001 to 1.000%,
Ti: 0 to 0.200%,
V: 0 to 0.300%,
Cu: 0 to 0.40%,
Cr: 0 to 0.90%,
Mo: 0 to 0.12%,
Ni: 0 to 0.30%,
B: 0 to 0.0030%,
Ca: 0 to 0.0010%,
Mg: 0 to 0.0010%,
Bi: 0 to 0.010%,
Zr: 0 to 0.050%,
Co: 0 to 0.010%,
Zn: 0 to 0.010%,
W: 0 to 0.100%,
Sn: 0 to 0.040%,
As: 0 to 0.100%,
REM: 0 to 0.0100%, and
balance: Fe and impurities, and
a microstructure comprising, by area%,
martensite: 90.0% or more, and
retained austenite: 3.0% or less, wherein
a mean particle size of prior austenite grains is 30.0 µm or less, and
when defining a region surrounded by grain boundaries with an orientation difference
of 15° or more in the martensite as a "crystal grain", a ratio of crystal grains with
an orientation difference in the grains of 4° or more is, by area%, 45.0 to 70.0%.
[0013] As explained previously, it is known that along with an increase in the strength
of a steel material, the hole expandability and other properties fall. For example,
to produce a part having a complicated shape such as a lower arm, trailing arm, etc.,
among the transmission parts of an automobile, a steel sheet securing a high strength,
in particular high strength of a tensile strength of 980 MPa or more enabling reduction
of weight, while having excellent hole expandability is being sought. From the viewpoint
of raising the strength, the microstructure of the steel sheet is preferably made
a structure mainly comprised of martensite. However, martensitic steel has a layered
structure including packets, blocks, laths, and other substructures in the prior austenite
grains. While excellent in strength, in general, there is a problem of a low workability.
For this reason, in forming operations performed divided into several steps such as
press-forming, due to the work hardening caused by strain introduced in the initial
period of deformation, in the latter period of deformation, the workability generally
falls. Therefore, a steel sheet able to realize both high strength and workability
by exhibiting a high work hardening ability even in the latter period of deformation
of press-forming is being sought.
[0014] Therefore, the inventors engaged in studies focusing in particular on the microstructure
of the hot rolled steel sheet in addition to prescribing a suitable chemical composition
of the steel sheet, in particular the hot rolled steel sheet. First, the inventors
discovered that by making the microstructure of hot rolled steel sheet having a predetermined
chemical composition a structure mainly comprised of martensite, more specifically,
a structure containing, by area%, martensite: 90.0% or more and retained austenite:
3.0% or less, it is possible to achieve high strength, for example, high strength
of a tensile strength of 980 MPa or more, while remarkably improving the hole expandability
of the hot rolled steel sheet. While not intending to be bound by any specific theory,
it is believed that by making the microstructure a more uniform structure comprising
martensite in an area% of 90.0% or more, it is possible to reduce the hardness difference
in the microstructure compared with the case where other structures softer than martensite,
for example, ferrite, etc., are contained in relatively large amounts and that due
to such reduction of the hardness difference, the hole expandability can be improved.
Further, retained austenite can become starting points for fracture during deformation
in press-forming, etc., and therefore by limiting the retained austenite to an area%
of 3.0% or less in addition to controlling the martensite to an area% of 90.0% or
more, the hole expandability can be improved more remarkably.
[0015] Next, since it is believed prior austenite grain boundaries act as resistance against
motion of dislocations and would be effective for improving work hardening ability,
the inventors studied improvement of the work hardening ability from the viewpoint
of making the particle size of the prior austenite grains in a microstructure mainly
comprised of martensite a suitable one. More specifically, by making the prior austenite
grains finer, it is possible to increase the density of prior austenite grain boundaries.
For this reason, it is possible to increase the obstacles to dislocation by making
the prior austenite grains finer and therefore it becomes possible to raise the work
hardening ability. However, if just making the prior austenite grains finer, for example,
sometimes a sufficient work hardening ability cannot be exhibited in a latter period
of deformation of a forming operation such as press-forming performed divided into
several steps. Therefore, the inventors took note of control of the form of the martensite
structure in addition to control of the particle size in prior austenite grains and
studied the same. As a result, the inventors discovered that by making the prior austenite
grains finer within a predetermined range, more specifically controlling the mean
particle size of prior austenite grains to 30.0 µm or less, the work hardening ability
of the hot rolled steel sheet as a whole is improved while by suitably controlling
the ratio of specific crystal grains in the martensite structure, more specifically,
when defining a region surrounded by grain boundaries with an orientation difference
of 15° or more in the martensite as a "crystal grain", by controlling a ratio of crystal
grains with an orientation difference in the grains of 4° or more to a range of, by
area%, 45.0 to 70.0%, it is possible to achieve a high work hardening rate even in
a state where a certain extent of strain is introduced such as at the latter period
of press-forming.
[0016] While not intending to be bound by any specific theory, by controlling the ratio
of crystal grains with an orientation difference in the grains of 4° or more in the
martensite to a range of, by area%, 45.0 to 70.0%, it is possible to form a martensite
structure with dislocations unevenly dispersed. It is believed that such a martensite
structure contributes to a high work hardening rate in the latter period of deformation
in press-forming, etc. More specifically, the orientation difference in the crystal
grains expresses the state of dispersion of dislocations. The more unevenly the dislocations
are dispersed, generally the greater the orientation difference in the grains becomes.
Therefore, by including crystal grains raised in orientation difference in the grains
in the martensite in a suitable ratio and establishing the presence of a certain amount
of a structure with dislocations unevenly dispersed, uneven deformation occurs during
press-forming and other working. As a result, even in the latter period of deformation,
a sufficient work hardening ability can be maintained and therefore it is believed
a high work hardening rate can be achieved. In particular, crystal grains with an
orientation difference in the grains of 4° or more are crystal grains sufficient for
causing uneven deformation. By controlling such crystal grains to within a range of,
by area%, 45.0 to 70.0%, it becomes possible to achieve the desired work hardening
rate. Therefore, even at a location receiving primary deformation in for example press-forming,
etc., and accumulating strain inside the steel sheet and, in that state, again receiving
separate deformation (stretch flange deformation, etc.), according to the steel sheet
according to an embodiment of the present invention, it becomes possible to stably
form the structure for maintaining a high work hardening ability. The fact that in
a microstructure mainly comprised of martensite, by controlling the ratio of the crystal
grains with a raised orientation difference in the grains to within a predetermined
range and forming a structure with dislocations unevenly dispersed, it is possible
to improve the work hardening ability of the steel sheet has not been conventionally
known and was first made clear this time by the inventors. As a result, according
to the steel sheet according to an embodiment of the present invention, for example,
despite being a high strength of a tensile strength of 980 MPa or more, the hole expandability
and work hardening ability can be remarkably improved. Therefore, the steel sheet
according to an embodiment of the present invention can reliably achieve the contradictory
properties of high strength and excellent workability, and therefore is particularly
useful in use in the automotive field where realization of both of these properties
is sought.
[0017] Below, the steel sheet according to an embodiment of the present invention will be
explained in more detail. In the following explanation, the "%" of the units of contents
of the elements, unless otherwise indicated, means "mass%". Further, in this Description,
the "to" showing a numerical range, unless otherwise indicated, is used in the sense
of the numerical values described before and after the same being included as the
lower limit value and the upper limit value.
[C: 0.040 to 0.200%]
[0018] C is an element effective for raising the strength of steel sheet. Further, C forms
carbides and/or carbonitrides with Nb in the steel and contributes to refinement of
the structure by the pinning effect of the precipitates formed. To sufficiently obtain
these effects, the C content is 0.040% or more. The C content may also be 0.060% or
more, 0.080% or more, 0.100% or more, or 0.120% or more. On the other hand, if excessively
containing C, sometimes the workability falls. Therefore, the C content is 0.200%
or less. The C content may also be 0.180% or less, 0.160% or less, 0.150% or less,
or 0.140% or less.
[Si: 0.30 to 2.00%]
[0019] Si is an element effective for raising the strength as a solution strengthening element.
To sufficiently obtain such an effect, the Si content is 0.30% or more. The Si content
may also be 0.40% or more, 0.50% or more, 0.60% or more, 0.70% or more, 0.85% or more,
1.00% or more, or 1.20% or more. On the other hand, if excessively containing Si,
the chemical convertability and workability fall and during hot rolling, slab cracking
sometimes occurs. Therefore, the Si content is 2.00% or less. The Si content may also
be 1.80% or less, 1.60% or less, 1.50% or less, or 1.40% or less.
[Mn: 1.00 to 4.00%]
[0020] Mn is an element effective for raising the hardenability and the strength as a solution
strengthening element. To sufficiently obtain these effects, the Mn content is 1.00%
or more. The Mn content may also be 1.20% or more, 1.50% or more, 1.80% or more, 2.00%
or more, or 2.20% or more. On the other hand, if excessively containing Mn, the workability
sometimes falls. Therefore, the Mn content is 4.00% or less. The Mn content may also
be 3.80% or less, 3.50% or less, 3.20% or less, 3.00% or less, or 2.80% or less.
[sol. Al: 0.001 to 0.500%]
[0021] sol. Al is an element acting as a deoxidizer of molten steel. Further, sol. Al is
an element suppressing the precipitation of the cementite so harmful to hole expandability.
To obtain these effects, the sol. Al content is 0.001% or more. The sol. Al content
may also be 0.010% or more, 0.020% or more, 0.030% or more, 0.050% or more, or 0.100%
or more. On the other hand, even if excessively containing sol. Al, the effect becomes
saturated and a rise in production costs is liable to be invited. Therefore, the sol.
Al content is 0.500% or less. The sol. Al content may also be 0.400% or less, 0.300%
or less, or 0.200% or less. "sol. Al" means acid soluble Al and indicates solid solution
Al present in the steel in a solid solution state.
[P: 0.100% or Less]
[0022] If P is excessively contained, sometimes grain boundary segregation, etc., causes
the workability to fall. Therefore, the P content is 0.100% or less. The P content
may also be 0.050% or less, 0.030% or less, 0.020% or less, or 0.015% or less. The
lower limit of the P content is not particularly prescribed and may also be 0%, but
excessive reduction would invite a rise in costs. Therefore, the P content may also
be 0.0001% or more, 0.001% or more, or 0.005% or more.
[S: 0.0300% or Less]
[0023] If S is excessively contained, sometimes MnS and other sulfides are formed in large
amounts and the workability is made to fall. Therefore, the S content is 0.0300% or
less. The S content may also be 0.0200% or less, 0.0100% or less, or 0.0050% or less.
The lower limit of the S content is not particularly prescribed and may also be 0%,
but excessive reduction would invite a rise in costs. Therefore, the S content may
also be 0.0001% or more, 0.0010% or more, or 0.0030% or more.
[N: 0.0070% or Less]
[0024] If N is excessively contained, sometimes coarse nitrides are formed and the workability
is made to fall. Therefore, the N content is 0.0070% or less. The N content may also
be 0.0050% or less, 0.0040% or less, or 0.0030% or less. The lower limit of the N
content is not particularly prescribed and may also be 0%, but excessive reduction
would invite a rise in costs. Therefore, the N content may also be 0.0001% or more
or 0.0005% or more.
[O: 0.0100% or Less]
[0025] O is an element entering in the production process. If excessively containing O,
coarse inclusions are formed and the workability of the steel sheet is liable to fall.
Therefore, the O content is 0.0100% or less. The O content may also be 0.0080% or
less, 0.0060% or less, or 0.0040% or less. The lower limit of the O content is not
particularly prescribed and may also be 0%, but reduction to less than 0.0001% would
require time for refining and invite a drop in productivity. Therefore, the O content
may also be 0.0001% or more or 0.0005% or more.
[Nb: 0.001 to 1.000%]
[0026] Nb is an element forming carbides, nitrides, and/or carbonitrides in the steel and
contributes to refinement of the structure of the retained austenite grains and in
turn higher strength of the steel sheet by the pinning effect. To sufficiently obtain
these effects, the Nb content is 0.001% or more. The Nb content may also be 0.005%
or more, 0.010% or more, 0.050% or more, 0.100% or more, 0.200% or more, or 0.300%
or more. On the other hand, if excessively containing Nb, coarse carbides, etc., are
formed in the steel and the workability of the steel sheet sometimes falls. Therefore,
the Nb content is 1.000% or less. The Nb content may also be 0.800% or less, 0.600%
or less, or 0.500% or less.
[0027] The basic chemical composition of the steel sheet according to an embodiment of the
present invention is as explained above. Furthermore, the steel sheet may, according
to need, further contain at least one of the following elements in place of part of
the balance of Fe.
[Cr: 0 to 0.90%]
[0028] Cr is an element raising the hardenability of steel and contributing to improvement
of the strength and/or corrosion resistance. The Cr content may also be 0%, but to
obtain these effects, the Cr content is preferably 0.001% or more and may also be
0.01% or more, 0.05% or more, or 0.10% or more. On the other hand, even if excessively
containing Cr, the effect becomes saturated and a rise in production costs is liable
to be invited. Therefore, the Cr content is preferably 0.90% or less and may also
be 0.70% or less, 0.50% or less, 0.40% or less, or 0.30% or less.
[Ti: 0 to 0.200%, V: 0 to 0.300%, Cu: 0 to 0.40%, Mo: 0 to 0.12%, Ni: 0 to 0.30%,
B: 0 to 0.0030%, Ca: 0 to 0.0010%, Mg: 0 to 0.0010%, Bi: 0 to 0.010%, Zr: 0 to 0.050%,
Co: 0 to 0.010%, Zn: 0 to 0.010%, W: 0 to 0.100%, Sn: 0 to 0.040%, As: 0 to 0.100%,
and REM: 0 to 0.0100%]
[0029] Ti, V, Cu, Mo, Ni, B, Ca, Mg, Bi, Zr, Co, Zn, W, Sn, As, and REM may be contained
in the steel sheet as optional elements or sometimes are present in the steel sheet
as trump elements. The contents of these elements may also be Ti: 0 to 0.200%, or
0.100%, V: 0 to 0.300%, or 0.200%, Cu: 0 to 0.40%, or 0.20%, Mo: 0 to 0.12% or 0.08%,
Ni: 0 to 0.30%, or 0.15%, B: 0 to 0.0030%, or 0.0015%, Ca: 0 to 0.0010%, or 0.0008%,
Mg: 0 to 0.0010%, or 0.0008%, Bi: 0 to 0.010%, Zr: 0 to 0.050%, or 0.030%, Co: 0 to
0.010%, Zn: 0 to 0.010%, W: 0 to 0.100%, or 0.050%, Sn: 0 to 0.040%, or 0.020%, As:
0 to 0.100%, or 0.050%, and REM: 0 to 0.0100%, or 0.0050%. Regarding the lower limit
values of these elements, for example, the Ti, V, Cu, Mo, Ni, Bi, Zr, Co, Zn, W, Sn,
and As contents may also be 0.001% or more, 0.005% or more, or 0.008% or more. Similarly,
the B, Ca, Mg and REM content may also be 0.0001% or more, 0.0002% or more, or 0.0005%
or more.
[0030] In the steel sheet according to an embodiment of the present invention, the balance
besides the above-mentioned elements is comprised of Fe and impurities. The "impurities"
are constituents, etc., entering from ore, scrap, and other such starting materials
due to various factors in the production process when, for example, industrially producing
the steel sheet. They are allowed to be included in a range not affecting the effect
of the present invention.
[0031] The chemical composition of the steel sheet according to an embodiment of the present
invention may be measured by a general analysis method. For example, the chemical
composition of the steel sheet may be measured by inductively coupled plasma-atomic
emission spectrometry (ICP-AES). C and S can be measured using the combustion-infrared
absorption method, N using the inert gas melting-thermal conductivity method, and
O using the inert gas melting-nondispersive type infrared absorption method.
[Microstructure]
[Martensite: 90.0% or More and Retained Austenite: 3.0% or Less]
[0032] The microstructure of the steel sheet according to an embodiment of the present invention
includes, by area%, martensite: 90.0% or more and retained austenite: 3.0% or less.
By configuring the microstructure of the steel sheet to include these structures,
it is possible to achieve high strength, for example, high strength of a tensile strength
of 980 MPa or more, while remarkably improving the hole expandability of the obtained
steel sheet. More specifically, by controlling the hard martensite to a range of,
by area%, 90.0% or more to obtain a more uniform structure, not only is higher strength
contributed to, but also the hardness difference in the microstructure can be reduced.
Due to such reduction of the hardness difference, the hole expandability can be improved.
If the area ratio of the martensite is less than 90.0%, the desired strength and hole
expandability cannot be achieved. From the viewpoint of further higher strength and
improved hole expandability, the higher the area ratio of martensite, the more preferable.
For example, it may be 92.0% or more, 94.0% or more, 96.0% or more, or 98.0% or more.
The upper limit of the area ratio of martensite is not particularly prescribed and
may also be 100.0%. For example, it may be 99.0% or less. On the other hand, retained
austenite can form starting points for fracture during deformation in press-forming,
etc., and therefore by controlling the martensite to an area% of 90.0% or more plus
controlling the retained austenite to an area% of 3.0% or less, it becomes possible
to more remarkably improve the hole expandability. If the area ratio of the retained
austenite is more than 3.0%, the grains form starting points for fracture during deformation
and the hole expandability falls. From the viewpoint of further improving the hole
expandability, the lower the area ratio of the retained austenite, the more preferable.
For example, it may be 2.5% or less, 2.0% or less, 1.5% or less, or 1.0% or less.
The lower limit of the area ratio of the retained austenite is not particularly limited
and may be 0%. For example, it may be 0.5% or more.
[Balance Structures]
[0033] The balance structures besides the martensite and retained austenite may be an area%
of 0%, but if there are balance structures present, the balance structures may include
at least one of ferrite: 10.0% or less, bainite: 10.0% or less, and pearlite: 10.0%
or less. If the area ratio of the at least one of ferrite, bainite, and pearlite is
a total of more than 10.0%, the area ratio of martensite becomes less than 90.0%,
and therefore as a result the desired strength and hole expandability can no longer
be achieved. The lower limits of ferrite, bainite, and pearlite may respectively be
0%. For example, they are respectively 0.1% or more, 0.5% or more, 1.0% or more, 2.0%
or more, or 3.0% or more. Similarly, the upper limits of ferrite, bainite, and pearlite
may be respectively 8.0% or less, 6.0% or less, 5.0% or less, or 4.0% or less.
[Identification of Microstructure and Calculation of Area Ratios]
[0034] The microstructure in steel sheet is identified and the area ratios are calculated
by examination under an optical microscope and X-ray diffraction after corrosion using
a Nital reagent or LePera solution. The structure is examined under an optical microscope
at a sheet thickness cross-section in a direction vertical to the sheet surface. Note
that the sheet thickness cross-section is preferably parallel to the rolling direction.
Specifically, first, a sample is taken from the steel sheet and examined surface of
the sample is etched by Nital. Next, an optical microscope is used to photograph a
300 µm×300 µm field at the 1/4 depth position of sheet thickness. The obtained structural
photograph is analyzed to calculate the total area of the martensite and bainite and
the individual area ratios of ferrite and pearlite. Next, the sample with the examined
surface corroded by the LePera solution is used and an optical microscope is similarly
used to photograph a 300 µm×300 µm field at the 1/4 depth position of sheet thickness.
The obtained structural photograph is analyzed to calculate the total area ratio of
martensite and retained austenite. Next, a sample ground at its surface down to 1/4
depth of sheet thickness from the logarithmic direction of the rolled surface is used
to calculate the volume ratio of the retained austenite by X-ray diffraction measurement.
The volume ratio of retained austenite is equal to the area ratio, and therefore this
is deemed the area ratio of the retained austenite. The obtained area ratio of retained
austenite is subtracted from the total area ratio of martensite and retained austenite
similarly calculated previously to calculate the area ratio of martensite. Finally,
the obtained area ratio of martensite is subtracted from the total area ratio of martensite
and bainite similarly calculated in in advance to thereby calculate the area ratio
of the bainite.
[Mean Particle Size of Prior Austenite Grains: 30.0 µm or Less]
[0035] In the steel sheet according to an embodiment of the present invention, the mean
particle size of the prior austenite grains is 30.0 µm or less. As explained previously,
prior austenite grain boundaries act as resistance to motion of dislocations and are
believed effective for improvement of the work hardening ability. In relation to this,
by refining the prior austenite grains, it is possible to increase the density of
the prior austenite grain boundaries. For this reason, by refining the prior austenite
grains to 30.0 µm or less, it is possible to increase the obstacles to dislocation
and therefore possible to raise the work hardening ability of the obtained steel sheet.
From the viewpoint of further raising the work hardening ability of the steel sheet,
the smaller the mean particle size of the prior austenite grains, the more preferable.
For example, it may be 28.0 µm or less, 25.0 µm or less, 22.0 µm or less, 20.0 µm
or less, 18.0 µm or less, or 15.0 µm or less. The lower limit is not particularly
prescribed, but the mean particle size of the prior austenite grains may be, for example,
3.0 µm or more, 5.0 µm or more, 8.0 µm or more, 10.0 µm or more, or 12.0 µm or more.
[Ratio of Prior Austenite Grains With Aspect Ratio of 2.0 or Less in All Prior Austenite
Grains: By Area% 90.0% or More]
[0036] In the microstructure of a steel sheet according to an embodiment of the present
invention, while not particularly limited to this, the ratio of prior austenite grains
with an aspect ratio of 2.0 or less in all prior austenite grains may be an area%
of for example 90.0% or more, 92.0% or more, 94.0% or more, or 96.0% or more. By making
the ratio of the prior austenite grains having a relatively small aspect ratio greater,
it is possible to reduce the anisotropy of the microstructure. The upper limit is
not particularly prescribed, but for example the ratio of prior austenite grains with
an aspect ratio of 2.0 or less in all prior austenite grains may be 100.0% and may
also be 99.0% or less or 98.0% or less. The present invention, as mentioned above,
has as its object the provision of steel sheet which, while high strength, is improved
in hole expandability and work hardening ability. It achieves the above object by
making the microstructure of steel sheet having a predetermined chemical composition
a structure mainly comprised of martensite and limiting the mean particle size of
prior austenite grains in the microstructure to within a predetermined range while
suitably controlling the ratio of crystal grains having a predetermined grain orientation
difference in the martensite structure. Therefore, it is clear that the ratio of prior
austenite grains with an aspect ratio of 2.0 or less in all prior austenite grains
is not a technical feature essential in achieving the object of the present invention.
[Methods of Determination of Mean Particle Size of Prior Austenite Grains and Ratio
of Prior Austenite Grains With Aspect Ratio of 2.0 or Less in All Prior Austenite
Grains]
[0037] The mean particle size of prior austenite grains and the ratio of prior austenite
grains with an aspect ratio of 2.0 or less in all prior austenite grains are determined
in the following way. First, a sample is cut out from any position 50 mm or more away
from the end faces of the steel sheet (if not possible to take a sample from that
position, a position avoiding the end parts) so that a vertical sheet thickness cross-section
can be examined. The sheet thickness cross-section is preferably parallel to the rolling
direction. The size of the sample, while depending on the measurement device, is made
a size enabling examination of about 10 mm in the direction vertical to the sheet
thickness direction. The cross-section of the sample is polished using #600 to #1500
silicon carbide paper, then is finished to a mirror surface using particle size 1
to 6 µm diamond powder made to disperse in alcohol or other diluent or pure water.
Next, electrolytic polishing is used to finish the examined surface. At the 1/4 depth
position of sheet thickness at any position in the longitudinal direction of the sample
cross-section, a length 50 µm and sheet thickness direction 50 µm region is measured
by electron backscatter diffraction at 0.1 µm measurement intervals to obtain crystal
orientation information. For the measurement, an EBSD analysis apparatus comprised
of a thermal field emission type scan electron microscope and EBSD detector may be
used. For example, an EBSD analysis apparatus comprised of a JSM-7001F made by JEOL
and a DVC5 type detector made by TSL may be used. At that time, the vacuum degree
inside the EBSD analysis apparatus may be 9.6×10
- 5 Pa or less, the acceleration voltage may be 15 kV, and the probe current level may
be 13. The obtained crystal orientation information is used to calculate the crystal
orientation of the prior austenite grains from the crystal orientation relationship
of general prior austenite grains and crystal grains having a body centered structure
after transformation. For the method of calculating the crystal orientation of prior
austenite grains, the following method is used. First, the method described in
Acta Materialia, 58(2010), 6393-6403 is used to prepare a crystal orientation map of the prior austenite grains. At one
of the prior austenite grains contained in the examined field, the average value of
the shortest diameter and the longest diameter is calculated. The average value is
made the particle size of the prior austenite grains. The above operation is performed
for all of the prior austenite grains except for the prior austenite grains not contained
in the photographed field in the entireties of the crystal grains such as at the end
parts of the photographed field. The particle size of all of the prior austenite grains
in the photographed field is sought. The mean particle size is determined by calculating
the mean particle size from the particle sizes of all of the prior austenite grains
obtained.
[0038] Next, at one of the prior austenite grains contained in the examined field, the ratio
of the diameter in the sheet thickness direction and diameter in the rolling direction
(rolling direction diameter/sheet thickness direction diameter) is calculated and
that value is used as the aspect ratio of the prior austenite grains. If the rolling
direction is unclear, the cross-section is examined at a direction of 0°, 45°, 90°,
and 135° with respect to any direction, the cross-section with the highest aspect
ratio among them is deemed the cross-section parallel to the rolling direction, and
the ratio of the diameter in the sheet thickness direction and diameter in the rolling
direction (rolling direction diameter/sheet thickness direction diameter) is calculated.
The above operation is performed for all of the prior austenite grains except for
the prior austenite grains not contained in the photographed field in the entireties
of the crystal grains such as at the end parts of the photographed field. The aspect
ratio of all of the prior austenite grains in the photographed field is sought. The
total number of the prior austenite grains with an aspect ratio of 2.0 or less divided
by the number of all prior austenite grains, the ratio of prior austenite grains with
an aspect ratio of 2.0 or less in all prior austenite grains is determined.
[Ratio of Crystal Grains With Orientation Difference in Grains in Martensite of 4°
or More: Area% 45.0 to 70.0%]
[0039] In the martensite structure of the steel sheet according to an embodiment of the
present invention, if a region surrounded by grain boundaries with an orientation
difference of 15° or more is defined as a "crystal grain", the ratio of crystal grains
with an orientation difference in the grains of 4° or more is controlled to a range
of, by area%, 45.0 to 70.0%. As explained earlier, the more unevenly dislocations
are dispersed, generally the greater the orientation difference in the grains becomes.
Crystal grains with an orientation difference in the grains of 4° or more are crystal
grains having an orientation difference sufficient for forming a structure with dislocations
unevenly dispersed and causing spread of uneven deformation. In relation to this,
in an embodiment of the present invention, by making such crystal grains form in the
martensite a range of, by an area%, 45.0 to 70.0% to establish the presence of a certain
amount of a structure with dislocations unevenly dispersed, uneven deformation occurs
in the press-forming or other working. As a result, it is possible to maintain a sufficient
work hardening ability even at the latter period of deformation and therefore possible
to achieve a high work hardening rate. If the ratio of crystal grains with an orientation
difference in the grains of 4° or more is an area% of less than 45.0% or more than
70.0%, uneven deformation becomes harder to develop during press-forming or other
working and therefore the desired work hardening rate becomes impossible to achieve.
The ratio of crystal grains with an orientation difference in the grains in the martensite
structure of 4° or more may be for example an area% of 48.0% or more, 50.0% or more,
or 55.0% or more. Similarly, the ratio of crystal grains with an orientation difference
in the grains in the martensite structure of 4° or more may also be for example an
area% of 65.0% or less, 62.0% or less, or 60.0% or less.
[Method of Determination of Ratio of Crystal Grains With Orientation Difference in
Grains of 4° or More in Martensite]
[0040] The ratio of crystal grains with an orientation difference in the grains of 4° or
more in the martensite is measured by electron backscatter diffraction (EBSD). More
specifically, first, a sample is taken from the steel sheet so that a sheet thickness
cross-section in a direction vertical to the sheet surface can be examined. At the
1/4 depth position of sheet thickness from the steel sheet surface, a region of 200
µm in the direction vertical to the sheet thickness direction and 100 µm region in
the sheet thickness direction is measured by EBSD at 0.2 µm measurement intervals
to obtain crystal orientation information. Here, an EBSD analysis apparatus comprised
of a thermal field emission type scan electron microscope (JSM-7001F made by JEOL)
and EBSD detector (HIKARI detector made by TSL) is used for analysis at a speed of
50 to 300 points/s. At that time, the vacuum degree inside the EBSD analysis apparatus
may be 9.6×10
-5 Pa or less, the acceleration voltage may be 15 kV, and the probe current level may
be 13. Next, the obtained crystal orientation information is used to identify the
martensite structure using a "Phase Map" function installed in the "OIM Analysis
®" software attached to the EBSD analysis apparatus. Next, defining a region surrounded
by grain boundaries with an orientation difference of 15° or more in the identified
martensite structures as a "crystal grain", the average orientation difference in
the grains of the crystal grains is calculated and the ratio of crystal grains with
an orientation difference in the grains of 4° or more is found. The crystal grains
defined as explained above and the average orientation difference in the grains can
similarly be calculated using the "OIM Analysis
®" software attached to the EBSD analysis apparatus. In the present invention, the
"orientation difference in the grains" expresses the dispersion of the orientations
in a crystal grain called the "grain orientation spread (GOS)". The value of the orientation
difference in the grains, as described in "
Analysis of Misorientation in Plastic Deformation of Stainless Steel by EBSD Method
and X-Ray Diffraction Method", Hidehiko Kimura et al., Transactions of the Japan Society
of Mechanical Engineers (A), vol. 71, no. 712, 2005, p. 1722-1728, is found as the average value of misorientation of all measurement points from the
crystal orientation used as a reference in the same crystal grain. In this embodiment
of the present invention, the crystal orientation used as the reference is the orientation
obtained by averaging all measurement points in the same crystal grain. The value
of GOS can be calculated using the "OIM Analysis
® Version 7.0.1" software attached to the EBSD analysis apparatus.
[Sheet Thickness]
[0041] The steel sheet according to an embodiment of the present invention is not particularly
limited, but in general it has a 1.0 to 8.0 mm sheet thickness. For example, the sheet
thickness may also be 1.2 mm or more, 1.6 mm or more, or 2.0 mm or more and/or may
also be 7.0 mm or less, 6.0 mm or less, 5.5 mm or less, 5.0 mm or less, 4.4 mm or
less, 4.2 mm or less, or 4.0 mm or less.
[0042] The steel sheet according to an embodiment of the present invention can reliably
realize the contradictory properties of high strength and excellent workability and
is useful for use for parts in technical fields in which achievement of both of these
properties is sought, etc. In particular, it is useful for use for parts in the automotive
field, etc. For this reason, in a preferred embodiment, an auto part including steel
sheet according to an embodiment of the present invention, in particular, a transmission
of an automobile, is provided. As examples of transmission parts of automobiles, a
lower arm, trailing arm, etc., may be mentioned. These auto parts, in particular transmission
parts of automobiles, need only contain the steel sheet according to an embodiment
of the present invention in at least portions of these parts. For this reason, at
least portions of these parts satisfy the above features of the chemical composition
and structure. At portions of the steel sheet with relatively low degrees of working
in press-forming and other forming, the features of the steel sheet do not particularly
change before and after forming. Portions of the steel sheet with relatively low degrees
of working are judged by being flat in shape without being bent or otherwise deformed,
by being small in rate of change of sheet thickness, and other features.
[Mechanical Properties]
[Tensile Strength: TS]
[0043] According to the steel sheet having the above-mentioned chemical composition and
microstructure, in particular hot rolled steel sheet, it is possible to achieve a
high tensile strength, specifically a tensile strength of 980 MPa or more. The tensile
strength is preferably 1000 MPa or more, 1080 MPa or more, or 1180 MPa or more. According
to the steel sheet according to an embodiment of the present invention, despite having
such an extremely high tensile strength, it is possible to realize excellent hole
expandability and work hardening ability by a specific combination of the chemical
composition and microstructure explained above. The upper limit of the tensile strength
is not particularly prescribed, but, for example, the tensile strength of the steel
sheet is 1780 MPa or less, 1700 MPa or less, or 1600 MPa or less. The tensile strength
is measured by taking a JIS No. 5 test piece from an orientation (C direction) where
the longitudinal direction of the test piece becomes parallel to the rolling perpendicular
direction of the steel sheet and performing a tensile test based on JIS Z 2241: 2011.
For example, if it is difficult to obtain a JIS No. 5 test piece due to dimensional
restrictions, it is possible to use another test piece described in JIS Z 2241: 2011.
However, if the sheet thickness is less than 0.5 mm, 0.5 mm is made the lower limit
for performing suitable evaluation. For example, if it is difficult to obtain a JIS
No. 5 test piece due to dimensional restrictions and and it is also difficult to use
another test piece described in JIS Z 2241: 2011, it is possible to perform a micro
Vickers test based on JIS Z 2244-1: 2020 and use the value obtained by converting
that hardness (HV) to tensile strength. The sample used for the micro Vickers test
can be prepared by the same method as the sample for evaluation of the mean particle
size and aspect ratio of the prior austenite grains. The micro Vickers test may be
performed by measuring 30 points at the sheet thickness 1/4 position by a load of
500 gf and using the average value. The conversion can be performed by the following
formula:

[Hole Expansion Rate: λ]
[0044] According to the steel sheet having the above-mentioned chemical composition and
microstructure, it is possible to obtain a high hole expandability, specifically a
45% or more hole expansion rate. The hole expansion rate may be preferably 50% or
more, more preferably 60% or more or 70% or more. The upper limit of the hole expansion
rate is not particularly prescribed, but, for example, the hole expansion rate is
150% or less, 120% or less, or 100% or less. The hole expansion rate is determined
in the following way: First, a width 100 mm×length 100 mm test piece is taken from
the steel sheet and a punch hole (initial hole: hole diameter d0=10 mm) is prepared
using a punch tool with a punch diameter of 10 mm and die diameter of 10.25 to 11.5
mm (clearance 12.5%). Next, while set so that the burr became the die side, a 60°
conical punch is used to expand the initial hole until a crack passing through the
sheet thickness is formed. The hole diameter d1mm is measured at the time of cracking
and the hole expansion rate λ (%) of each test piece is found by the following formula.
This hole expansion test is conducted three times and the average value of the same
is determined as the hole expansion rate λ.

<Method of Production of Steel Sheet>
[0045] Next, a preferable method of production of steel sheet according to an embodiment
of the present invention will be explained. The following explanation is intended
to illustrate the characteristic method for producing the steel sheet according to
an embodiment of the present invention, particularly steel sheet having particularly
preferable properties, and is not intended to limit the steel sheet to one produced
by the method of production such as explained below. More specifically, below, production
of hot rolled steel sheet will be specifically shown, but the steel sheet according
to an embodiment of the present invention encompasses any steel sheet having the above
explained chemical composition and microstructure, i.e., not only hot rolled steel
sheet, but also cold rolled steel sheet, plated steel sheet, etc. Therefore, the following
description just simply explains one example of a preferable method of production
when the steel sheet according to an embodiment of the present invention is hot rolled
steel sheet.
[0046] The method of production of the steel sheet according to an embodiment of the present
invention comprises
heating a slab having the chemical composition explained above in relation to the
steel sheet and holding it in a temperature region of 1100°C or more for 6000 seconds
or more,
hot rolling including finish rolling of the slab, wherein the finish rolling satisfies
conditions of following (a) to (c):
- (a) a rolling reduction at a rolling pass at one stage before a last stage is 30 to
50% and a rolling reduction at a rolling pass at the last stage is 20 to 50%,
- (b) a total rolling reduction is 90% or more, and
- (c) a rolling temperature at the rolling pass at one stage before the last stage is
970 to 1100°C and a final rolling temperature is 960 to 1050°C,
starting cooling of the finish rolled steel sheet within 0.5 to 10.0 seconds after
completion of the hot rolling, then cooling the steel sheet down to a temperature
of 400°C or less within 20.0 seconds from the start of cooling,
coiling the cooled steel sheet in a temperature region of 400°C or less, and
imparting to the obtained steel sheet a strain becoming an absolute value of 0.16
to 1.40% at a sheet thickness 1/4 position of the steel sheet three times or more
while repeatedly switching between positive and negative. In the above-mentioned method
of production, the temperatures described for the slab and steel sheet respectively
mean the surface temperature of the slab and the surface temperature of the steel
sheet. Below, the steps will be explained in detail.
[Heating Step]
[0047] First, a slab having a chemical composition explained above in relation to the steel
sheet is heated and is held in a temperature region of 1100°C or more for 6000 seconds
or more. For the slab, using a slab obtained by continuous casting is preferable from
the viewpoint of productivity, but it is also possible to use a slab obtained by casting
and blooming. In accordance with need, these which are hot worked or cold worked may
also be used. In the present method of production, "holding in the temperature region
of 1100°C or more" includes not only the case of holding the temperature of the slab
at a 1100°C or more fixed temperature but encompasses the case of holding the temperature
of the slab while fluctuating in the temperature region of 1100°C or more. By holding
the slab at the temperature region of 1100°C or more for 6000 seconds or more, it
is possible to make the coarse carbides present in the structure completely dissolve
and possible to eliminate starting points of cracking. If the holding temperature
is less than 1100°C or the holding time is less than 6000 seconds, the coarse carbides
become incompletely dissolved. If the coarse carbides are incompletely dissolved,
in the cooling step explained later, due to the occurrence of ferrite or bainite transformation
starting from such carbides, the area ratio of martensite becomes less than 90.0%
and as a result it becomes no longer possible to obtain the desired strength and/or
hole expandability. The upper limit of the heating temperature of the slab is preferably
1300°C or less or 1200°C or less. Similarly, the upper limit of the holding time at
the temperature region of 1100°C or more is preferably 10000 seconds or less.
[Hot Rolling Step]
[Rough Rolling]
[0048] In the present method of production, for example, the heated slab may be rough rolled
before the finish rolling so as to adjust the sheet thickness, etc. The rough rolling
need only be able to secure the desired sheet bar dimensions. The conditions are not
particularly limited.
[(a) Rolling Reduction in Rolling Passes of One Stage Before Last Stage: 30 to 50%
and Rolling Reduction in Last Stage: 20 to 50%]
[0049] The heated slab or the slab additionally rough rolled in accordance with need is
next finish rolled. In the present method of production, the finish rolling is performed
using a tandem rolling mill comprised of several rolling stands, for example, five
or more rolling stands. In the present method of production, in the finish rolling
performed on the heated slab, the rolling reduction at each rolling pass at the last
two stages has to be suitably controlled. Specifically, the rolling reduction at the
rolling pass one stage before the last stage is controlled to 30 to 50% while the
rolling reduction at the rolling pass at the last stage is controlled to 20 to 50%.
By rolling by such a relatively high rolling reduction at each rolling pass at one
stage before the last stage and the last stage, recrystallization is promoted and
the microstructure can be made finer and in addition the ratio of prior austenite
grains with an aspect ratio of 2.0 or less in all prior austenite grains can be raised.
If the rolling reduction at the rolling pass at one stage before the last stage is
less than 30% and/or the rolling reduction at the rolling pass at the last stage is
less than 20%, recrystallization either is not completed or is not sufficiently promoted
and in the microstructure of the finally obtained steel sheet, sometimes the desired
mean particle size of the prior austenite grains sometimes cannot be reached and/or
the ratio of the prior austenite grains with an aspect ratio of 2.0 or less becomes
a relatively small value. If the desired mean particle size of the prior austenite
grains cannot be achieved, sufficient work hardening ability no longer can be obtained.
On the other hand, if the rolling reduction at each rolling pass of one stage before
the last stage and/or the last stage is too high, the rolling load becomes excessive
and the burden of the rolling mill and other facilities becomes higher. For this reason,
the rolling reduction at each rolling pass of one stage before the last stage and
the last stage is 50% or less. Preferably the rolling reduction at each rolling pass
of one stage before the last stage and the last stage is 45% or less.
[(b) Overall Rolling Reduction: 90% or More]
[0050] In the present method of production, the total rolling reduction in the final rolling
is controlled to 90% or more. The Mn contained in the steel is an element causing
a drop in the fracture energy of the grain boundaries, and therefore if there are
regions where Mn is locally concentrated, sometimes occurrence of cracking is promoted
at the time of plastic deformation in the press-forming, etc. There, from the viewpoint
of further improving the hole expandability, suppressing or reducing local concentration
of Mn would be effective. By controlling the total rolling reduction in finish rolling
to 90% or more, it is possible to make the Mn disperse in the steel and in turn suppress
or reduce the variation in Mn concentration in the steel, i.e., suppress or reduce
the local concentration of Mn. If the total rolling reduction in the finish rolling
is less than 90%, the variation in Mn concentration becomes relatively high and, sometimes,
locally Mn concentrates and growth of regions with reduced fracture energy cannot
be sufficiently suppressed. In addition, if the total rolling reduction in finish
rolling is less than 90%, the cumulative strain during the rolling becomes insufficient,
and therefore sometimes the recrystallization will not be completed or not be sufficiently
promoted and the desired mean particle size of prior austenite grains in the microstructure
of the finally obtained steel sheet will not be able to be achieved and/or the ratio
of the prior austenite grains with an aspect ratio of 2.0 or less will become a relatively
small value. The upper limit of the total rolling reduction in the finish rolling
is, for example, 99% or less or 98% or less. Here, the total rolling reduction in
the finish rolling is calculated by the following formula:
Total rolling reduction (%)=(sheet thickness before finish rolling-sheet thickness
after finish rolling)/sheet thickness before finish rolling× 100

[(c) Rolling Temperature at Rolling Pass of One Stage Before Last Stage: 970 to 1100°C,
Final Rolling Temperature: 960 to 1050°C]
[0051] In the present method of production, in addition to control of the rolling reduction
in each rolling pass of the latter two stages in finish rolling, the rolling temperature
at the rolling pass of one stage before the last stage (entry side temperature of
rolling pass of one stage before the last stage) and the final rolling temperature
(end temperature of finish rolling) are also extremely important in control of the
microstructure of the steel sheet. If the rolling temperature at the rolling pass
of one stage before the last stage is less than 970°C and/or the final rolling temperature
is less than 960°C, sometimes the recrystallization is not completed or is not sufficiently
promoted and the desired mean particle size of the prior austenite grains in the microstructure
of the finally obtained steel sheet cannot be achieved and/or sometimes the ratio
of prior austenite grains with an aspect ratio of 2.0 or less becomes a relatively
small value. If not able to achieve the desired mean particle size of the prior austenite
grains, a sufficient work hardening ability can no longer be obtained. On the other
hand, if the rolling temperature of the one stage before the last stage is more than
1100°C and/or the final rolling temperature is more than 1050°C, the prior austenite
grains become coarser and sometimes the desired mean particle size of the prior austenite
grains cannot be achieved. In this case as well, only naturally, sufficient work hardening
ability can no longer be obtained.
[Cooling Step]
[Time From After Completion of Hot Rolling Step to Start of Cooling: 0.5 to 10.0 Seconds]
[Time From Start of Cooling to Becoming 400°C or Less: 20.0 Seconds or Less]
[0052] The finish rolled steel sheet starts to be cooled in the next cooling step within
0.5 to 10.0 seconds after the completion of the hot rolling step, then is cooled down
to a temperature of 400°C or less within 20.0 seconds from the start of cooling. By
performing such cooling control, in the microstructure of the finally obtained steel
sheet, it is possible to achieve the desired mean particle size of the prior austenite
grains and the desired ratio of prior austenite grains with an aspect ratio of 2.0
or less.
[0053] If the time from the completion of the hot rolling step to the start of cooling is
less than 0.5 second, sometimes the recrystallization will not be completed or not
be sufficiently promoted and the desired mean particle size of prior austenite grains
in the microstructure of the finally obtained steel sheet will not be able to be achieved
and/or the ratio of the prior austenite grains with an aspect ratio of 2.0 or less
will not be able to be obtained. If the time from the completion of the hot rolling
step to the start of cooling is more than 10.0 seconds, grain growth will proceed
too much and the desired mean particle size of the prior austenite grains will no
longer be able to be obtained. As a result, in either case, it will become no longer
possible to achieve a sufficient work hardening ability in the steel sheet. On the
other hand, if the cooling time from the start of cooling down to 400°C or less is
more than 20.0 seconds or the cooling stop temperature is more than 400°C, ferrite,
bainite, and/or pearlite will be produced during the cooling and the area ratio of
martensite will become less than 90.0%. As a result, the desired strength and/or hole
expansion ability will no longer be able to be obtained.
[Coiling Step]
[0054] Next, the cooled steel sheet is coiled up at a temperature region of 400°C or less.
If the coiling temperature is more than 400°C, in the same way as the case of the
cooling step, ferrite, bainite and/or pearlite is formed, the area ratio of the martensite
becomes less than 90.0%, and as a result it becomes no longer possible to obtain the
desired strength and/or hole expandability.
[Strain Imparting Step]
[0055] Finally, the obtained steel sheet was given strain becoming an absolute value of
0.16 to 1.40% at a sheet thickness 1/4 position of the steel sheet three times or
more while repeatedly switching between positive and negative to thereby produce the
steel sheet. By repeatedly imparting such strain to the steel sheet, it is possible
to unevenly introduce dislocations inside the crystal grains of the martensite structure
and as a result control the ratio of crystal grains with an orientation difference
in the grains of 4° or more to a range of, by area%, 45.0 to 70.0%. If the absolute
value of the strain imparted is less than 0.16% or the number of times of imparting
strain is less than three times, the uneven introduction of dislocations in the crystal
grains becomes insufficient, and therefore the ratio of crystal grains with an orientation
difference in the grains of 4° or more becomes an area% of less than 45.0% and it
becomes no longer possible to achieve the desired work hardening rate. On the other
hand, if the absolute value of the strain impart becomes more than 1.40%, the accumulation
of dislocations at the crystal grains becomes excessive whereby the ratio of crystal
grains with an orientation difference in the grains of 4° or more becomes more than
an area% of 70.0% and similarly the desired work hardening rate can no longer be achieved.
The upper limit of the number of times of imparting strain is not particularly prescribed,
but from the viewpoint of productivity is preferably 10 times or less, 7 times or
less, or 5 times or less.
[0056] The martensite structure inherits the dislocations in the austenite grains before
transformation, and therefore in general the crystal grains of the martensite structure
formed from the nonrecrystallized austenite grains become high in value of orientation
difference in the grains while the crystal grains of the martensite structure formed
from the recrystallized austenite grains become low in value of orientation difference
in the grains. In the present method of production, as explained above, recrystallization
is promoted in the hot rolling step to make the structure finer whereby the mean particle
size of the prior austenite grains is controlled to 30.0 µm or less. However, in such
a case, martensite is formed from the recrystallized austenite grains, and therefore
the crystal grains of the martensite structure become low in value of the orientation
difference in the grains and the ratio of crystal grains with an orientation difference
in the grains of 4° or more can no longer be made an area% of 45.0 to 70.0%. Therefore,
in the present method of production, for the prior austenite structure, by suitably
controlling the conditions of the hot rolling step to make the prior austenite structure
a structure with recrystallization substantially or completely completed, it is possible
to refine the structure and improve the work hardening ability of the steel sheet
as a whole while by unevenly introducing dislocations in some of the crystal grains
of the martensite structure in the strain imparting step to suitably form the orientation
difference, it becomes possible to achieve a high work hardening rate even in a state
with a certain degree of strain introduced such as in the latter period of deformation
of press-forming.
[0057] The strain imparting step can be performed by any suitable method known to persons
skilled in the art. While not particularly limited to this, as such a method, for
example bending-unbending deformation by a tension leveler, etc., may be mentioned.
In this case, by changing the size of the rolls or the relative positional relationship
of the rolls with each other in the tension leveler and further the sheet thickness
of the steel sheet, etc., it is possible to easily change the absolute value of the
strain imparted. Therefore, by suitably controlling these parameters, it is possible
to easily impart the desired strain to the sheet thickness 1/4 position of the steel
sheet.
[0058] According to the steel sheet produced by above-mentioned method of production, by
configuring the microstructure by a more uniform structure containing an area% of
martensite: 90.0% or more and retained austenite: 3.0% or less, it is possible to
achieve a high strength, for example, a high strength of a tensile strength of 980
MPa or more, while remarkably improving the hole expandability due to the reduction
of the hardness difference, etc. Furthermore, by controlling the mean particle size
of the prior austenite grains in the microstructure to 30.0 µm or less, it becomes
possible to improve the work hardening ability of the steel sheet as a whole while
by controlling the ratio of crystal grains with an orientation difference in the grains
of 4° or more in the martensite to a range of, by area%, 45.0 to 70.0%, it becomes
possible to achieve a high work hardening rate even in a state where a certain extent
of strain is introduced such as in the latter period of deformation in press-forming.
Therefore, the steel sheet produced according to the above-mentioned method of production
can reliably achieve both the contradictory properties of high strength and excellent
workability, and therefore is particularly useful in use in the automotive field where
realization of both of these properties is sought.
[0059] Below, examples will be used to explain the present invention in more detail, but
the present invention is not limited to these examples in any way.
EXAMPLES
[0060] In the following examples, steel sheets according to an embodiment of the present
invention, in particular hot rolled steel sheets, were produced under various conditions
and investigated for the tensile strength (TS), hole expansion rate (λ), and work
hardening rate (WHR) of the obtained steel sheets.
[0061] First, molten steels were cast by the continuous casting method to form slabs having
the various chemical compositions shown in Tables 1 and 2. These slabs were heated
to 1100 to 1200°C in temperature and held over the time periods shown in Table 3,
then were hot rolled. The hot rolling was performed by rough rolling and finish rolling.
More specifically, the rough rolling was performed under the same conditions in all
of the examples and comparative examples while the finish rolling was performed under
the conditions shown in Table 3 using a tandem rolling mill comprised of five rolling
stands. Next, the finish rolled steel sheets were cooled and coiled under the conditions
shown in Table 3. Finally, strain was imparted to give an absolute value shown in
Table 3 at a sheet thickness 1/4 position of the steel sheet a predetermined number
of times while repeatedly switching between positive and negative.
[Table 1]
[0062]
Table 1
| Steel no. |
Chemical composition (mass%), balance of Fe and impurities |
Remarks |
| C |
Si |
Mn |
sol. Al |
P |
S |
N |
O |
Nb |
| A |
0.069 |
0.70 |
2.52 |
0.026 |
0.001 |
0.0007 |
0.0015 |
0.0035 |
0.023 |
Inv. steel |
| B |
0.042 |
1.80 |
3.14 |
0.466 |
0.005 |
0.0047 |
0.0026 |
0.0022 |
0.657 |
Inv. steel |
| C |
0.188 |
0.65 |
2.57 |
0.163 |
0.003 |
0.0019 |
0.0012 |
0.0046 |
0.238 |
Inv. steel |
| D |
0.120 |
0.31 |
2.96 |
0.364 |
0.024 |
0.0030 |
0.0009 |
0.0042 |
0.483 |
Inv. steel |
| E |
0.094 |
1.92 |
3.77 |
0.216 |
0.024 |
0.0055 |
0.0055 |
0.0048 |
0.525 |
Inv. steel |
| F |
0.097 |
1.69 |
1.22 |
0.137 |
0.015 |
0.0039 |
0.0036 |
0.0065 |
0.228 |
Inv. steel |
| G |
0.114 |
1.42 |
3.86 |
0.412 |
0.015 |
0.0026 |
0.0054 |
0.0040 |
0.525 |
Inv. steel |
| H |
0.050 |
1.17 |
2.89 |
0.003 |
0.010 |
0.0041 |
0.0032 |
0.0021 |
0.613 |
Inv. steel |
| I |
0.177 |
1.02 |
2.49 |
0.485 |
0.030 |
0.0018 |
0.0013 |
0.0051 |
0.220 |
Inv. steel |
| J |
0.123 |
1.02 |
2.19 |
0.015 |
0.020 |
0.0027 |
0.0020 |
0.0066 |
0.002 |
Inv. steel |
| K |
0.092 |
0.86 |
1.54 |
0.340 |
0.025 |
0.0014 |
0.0010 |
0.0006 |
0.904 |
Inv. steel |
| L |
0.130 |
1.02 |
1.87 |
0.061 |
0.023 |
0.0026 |
0.0044 |
0.0005 |
0.801 |
Inv. steel |
| M |
0.120 |
0.55 |
3.23 |
0.015 |
0.014 |
0.0051 |
0.0026 |
0.0022 |
0.461 |
Inv. steel |
| N |
0.076 |
0.81 |
1.94 |
0.261 |
0.022 |
0.0056 |
0.0035 |
0.0039 |
0.409 |
Inv. steel |
| O |
0.118 |
1.31 |
2.66 |
0.167 |
0.002 |
0.0028 |
0.0037 |
0.0070 |
0.458 |
Inv. steel |
| P |
0.074 |
0.68 |
1.77 |
0.226 |
0.028 |
0.0025 |
0.0037 |
0.0050 |
0.396 |
Inv. steel |
| Q |
0.112 |
1.78 |
2.78 |
0.309 |
0.019 |
0.0005 |
0.0052 |
0.0011 |
0.475 |
Inv. steel |
| R |
0.168 |
1.60 |
3.05 |
0.179 |
0.022 |
0.0032 |
0.0029 |
0.0006 |
0.565 |
Inv. steel |
| S |
0.182 |
0.65 |
2.23 |
0.231 |
0.027 |
0.0028 |
0.0007 |
0.0061 |
0.071 |
Inv. steel |
| T |
0.091 |
0.45 |
3.65 |
0.322 |
0.015 |
0.0017 |
0.0017 |
0.0027 |
0.764 |
Inv. steel |
| U |
0.122 |
1.82 |
3.29 |
0.424 |
0.008 |
0.0059 |
0.0063 |
0.0050 |
0.162 |
Inv. steel |
| V |
0.038 |
0.80 |
1.81 |
0.147 |
0.014 |
0.0058 |
0.0062 |
0.0005 |
0.144 |
Comp. steel |
| W |
0.211 |
0.65 |
2.96 |
0.408 |
0.011 |
0.0052 |
0.0027 |
0.0017 |
0.579 |
Comp. steel |
| X |
0.133 |
0.27 |
2.62 |
0.154 |
0.024 |
0.0048 |
0.0056 |
0.0041 |
0.508 |
Comp. steel |
| Y |
0.047 |
2.13 |
2.63 |
0.067 |
0.007 |
0.0037 |
0.0006 |
0.0015 |
0.659 |
Comp. steel |
| Z |
0.126 |
0.57 |
0.95 |
0.083 |
0.021 |
0.0043 |
0.0040 |
0.0015 |
0.096 |
Comp. steel |
| AA |
0.147 |
1.07 |
4.10 |
0.271 |
0.025 |
0.0032 |
0.0009 |
0.0046 |
0.768 |
Comp. steel |
| AB |
0.157 |
1.70 |
1.75 |
0.000 |
0.016 |
0.0037 |
0.0060 |
0.0070 |
0.276 |
Comp. steel |
| AC |
0.129 |
1.70 |
1.82 |
0.281 |
0.012 |
0.0014 |
0.0039 |
0.0043 |
0.000 |
Comp. steel |
| AD |
0.069 |
0.70 |
3.82 |
0.233 |
0.008 |
0.0005 |
0.0057 |
0.0048 |
1.021 |
Comp. steel |
| Underlines indicate outside scope of present invention. |
[Table 2]
[0063]
Table 2
| Steel no. |
Chemical composition (mass%), balance of Fe and impurities |
Remarks |
| Ti |
V |
Cu |
Cr |
Mo |
Ni |
B |
Ca |
Mg |
Bi |
Zr |
Co |
Zn |
W |
Sn |
As |
REM |
| A |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Inv. steel |
| B |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Inv. steel |
| C |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Inv. steel |
| D |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Inv. steel |
| E |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Inv. steel |
| F |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Inv. steel |
| G |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Inv. steel |
| H |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Inv. steel |
| I |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Inv. steel |
| J |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Inv. steel |
| K |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Inv. steel |
| L |
|
|
|
|
|
|
|
0.0005 |
0.0007 |
|
|
|
|
|
|
|
|
Inv. steel |
| M |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
0.0082 |
Inv. steel |
| N |
|
|
|
|
|
|
|
|
|
0.008 |
|
|
|
0.083 |
|
|
|
Inv. steel |
| O |
|
|
|
|
|
|
|
|
|
|
0.042 |
|
|
|
|
0.084 |
|
Inv. steel |
| P |
0.168 |
0.215 |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Inv. steel |
| Q |
|
|
0.33 |
|
|
|
|
|
|
|
|
0.006 |
|
|
|
|
|
Inv. steel |
| R |
|
|
|
0.54 |
|
|
|
|
|
|
|
|
|
|
|
|
|
Inv. steel |
| S |
|
|
|
|
0.08 |
|
|
|
|
|
|
|
|
|
0.037 |
|
|
Inv. steel |
| T |
|
|
|
|
|
0.20 |
|
|
|
|
|
|
|
|
|
|
|
Inv. steel |
| U |
|
|
|
|
|
|
0.0019 |
|
|
|
|
|
0.007 |
|
|
|
|
Inv. steel |
| V |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Comp. steel |
| W |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Comp. steel |
| X |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Comp. steel |
| Y |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Comp. steel |
| Z |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Comp. steel |
| AA |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Comp. steel |
| AB |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Comp. steel |
| AC |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Comp. steel |
| AD |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Comp. steel |
[Table 3]
[0064]
Table 3
| Production no. |
Steel no. |
Heating step |
Hot rolling step |
Cooling step |
Coiling step |
Strain imparting step |
Remarks |
| Holding time at 1100°C or more |
Rolling reduction of one stage before last stage |
Rolling temp. of one stage before last stage |
Rolling reduction of last stage |
Total rolling reduction |
Final rolling temp. |
Time until start of cooling |
Time from cooling start to 400°C or less |
Coiling temp. |
Absolute value of strain |
No. of times of imparting strain |
| s |
% |
°C |
% |
% |
°C |
s |
s |
°C |
% |
Times |
| 1 |
A |
8563 |
39 |
1052 |
41 |
95 |
1001 |
0.6 |
6.5 |
28 |
0.37 |
3 |
Inv. ex. |
| 2 |
A |
5922 |
44 |
999 |
48 |
91 |
968 |
2.4 |
8.9 |
26 |
0.79 |
3 |
Comp. ex. |
| 3 |
A |
8617 |
28 |
1052 |
39 |
91 |
1041 |
4.5 |
9.7 |
11 |
0.68 |
3 |
Comp. ex. |
| 4 |
A |
9693 |
46 |
965 |
44 |
98 |
960 |
3.0 |
7.2 |
19 |
0.99 |
5 |
Comp. ex. |
| 5 |
A |
7320 |
45 |
1108 |
48 |
96 |
1046 |
8.5 |
6.9 |
40 |
0.81 |
3 |
Comp. ex. |
| 6 |
A |
9613 |
35 |
1021 |
17 |
95 |
969 |
3.4 |
11.3 |
36 |
1.08 |
3 |
Comp. ex. |
| 7 |
A |
8630 |
39 |
973 |
43 |
94 |
953 |
5.6 |
11.3 |
30 |
1.09 |
4 |
Comp. ex. |
| 8 |
A |
7874 |
44 |
1098 |
42 |
92 |
1057 |
3.0 |
7.8 |
20 |
0.89 |
3 |
Comp. ex. |
| 9 |
A |
9552 |
45 |
1077 |
43 |
97 |
1048 |
0.2 |
9.5 |
31 |
0.62 |
3 |
Comp. ex. |
| 10 |
A |
7035 |
48 |
1072 |
45 |
91 |
1041 |
11.6 |
10.8 |
24 |
1.07 |
3 |
Comp. ex. |
| 11 |
A |
8506 |
39 |
1044 |
29 |
93 |
986 |
3.6 |
21.8 |
38 |
0.97 |
3 |
Comp. ex. |
| 12 |
A |
6994 |
39 |
980 |
41 |
93 |
964 |
2.9 |
11.5 |
414 |
0.54 |
3 |
Comp. ex. |
| 13 |
A |
7429 |
41 |
1034 |
39 |
96 |
975 |
5.8 |
9.0 |
11 |
0.13 |
3 |
Comp. ex. |
| 14 |
A |
7243 |
40 |
1021 |
24 |
92 |
972 |
1.8 |
8.1 |
24 |
1.50 |
3 |
Comp. ex. |
| 15 |
A |
7237 |
43 |
1034 |
35 |
92 |
1015 |
9.0 |
9.6 |
36 |
0.41 |
2 |
Comp. ex. |
| 16 |
A |
7229 |
42 |
1030 |
34 |
96 |
1000 |
9.1 |
9.3 |
34 |
0.00 |
0 |
Comp. ex. |
| 17 |
b |
6027 |
44 |
1000 |
46 |
95 |
993 |
5.9 |
10.1 |
34 |
0.54 |
3 |
Inv. ex. |
| 18 |
C |
9048 |
44 |
972 |
47 |
94 |
962 |
5.6 |
11.5 |
10 |
0.77 |
3 |
lnv. ex. |
| 19 |
D |
8932 |
40 |
1044 |
24 |
91 |
1000 |
7.9 |
9.7 |
269 |
0.58 |
3 |
Inv. ex. |
| 20 |
E |
9213 |
32 |
990 |
45 |
97 |
962 |
4.6 |
12.0 |
20 |
0.44 |
3 |
lnv. ex. |
| 21 |
F |
9515 |
35 |
1014 |
27 |
98 |
982 |
3.8 |
5.4 |
30 |
1.35 |
8 |
Inv. ex. |
| 22 |
G |
7031 |
41 |
1039 |
25 |
91 |
975 |
3.9 |
19.1 |
13 |
0.95 |
3 |
Inv. ex. |
| 23 |
H |
7074 |
48 |
986 |
41 |
94 |
963 |
3.3 |
8.9 |
26 |
0.46 |
6 |
Inv. ex. |
| 24 |
I |
8092 |
38 |
1036 |
34 |
96 |
1003 |
3.3 |
8.7 |
37 |
1.18 |
5 |
Inv. ex. |
| 25 |
J |
9290 |
41 |
1024 |
39 |
95 |
996 |
9.8 |
18.6 |
25 |
0.49 |
3 |
Inv. ex. |
| 26 |
K |
8048 |
42 |
1096 |
28 |
93 |
1048 |
7.4 |
7.1 |
11 |
0.98 |
3 |
Inv. ex. |
| 27 |
L |
7859 |
47 |
1067 |
47 |
94 |
1044 |
1.1 |
6.4 |
11 |
0.52 |
3 |
Inv. ex. |
| 28 |
M |
8653 |
45 |
1039 |
30 |
97 |
1025 |
6.4 |
10.8 |
30 |
1.10 |
3 |
Inv. ex. |
| 29 |
N |
9209 |
38 |
1019 |
40 |
91 |
985 |
8.3 |
10.7 |
20 |
0.32 |
3 |
Inv. ex. |
| 30 |
O |
8622 |
42 |
998 |
30 |
91 |
976 |
7.0 |
10.1 |
393 |
0.52 |
4 |
Inv. ex. |
| 31 |
P |
8141 |
46 |
1006 |
39 |
93 |
998 |
6.9 |
6.8 |
11 |
0.19 |
3 |
Inv. ex. |
| 32 |
Q |
8571 |
38 |
976 |
41 |
93 |
967 |
0.9 |
17.5 |
11 |
1.04 |
3 |
Inv. ex. |
| 33 |
R |
9773 |
47 |
996 |
21 |
95 |
973 |
6.3 |
9.0 |
39 |
1.13 |
3 |
Inv. ex. |
| 34 |
S |
6952 |
44 |
1028 |
38 |
96 |
973 |
5.1 |
10.3 |
24 |
0.58 |
3 |
Inv. ex. |
| 35 |
T |
7790 |
41 |
1068 |
27 |
98 |
1043 |
1.8 |
7.1 |
21 |
0.18 |
3 |
Inv. ex. |
| 36 |
U |
8502 |
40 |
981 |
28 |
95 |
979 |
1.9 |
9.9 |
13 |
0.92 |
3 |
Inv. ex. |
| 37 |
V. |
9297 |
42 |
1033 |
34 |
97 |
981 |
8.3 |
8.5 |
17 |
0.79 |
3 |
Comp. ex. |
| 38 |
W |
9293 |
37 |
1045 |
28 |
95 |
980 |
1.0 |
10.1 |
37 |
0.28 |
3 |
Comp. ex. |
| 39 |
X |
9263 |
37 |
1001 |
31 |
91 |
994 |
2.0 |
10.5 |
33 |
0.69 |
3 |
Comp. ex. |
| 40 |
Y |
7941 |
37 |
1012 |
27 |
91 |
990 |
4.0 |
6.1 |
40 |
0.95 |
6 |
Comp. ex. |
| 41 |
Z |
6635 |
47 |
1051 |
33 |
96 |
1041 |
7.0 |
8.1 |
28 |
0.44 |
3 |
Comp. ex. |
| 42 |
AA |
8547 |
43 |
983 |
41 |
97 |
960 |
9.0 |
9.0 |
31 |
0.66 |
3 |
Comp. ex. |
| 43 |
AB |
9730 |
42 |
1074 |
31 |
93 |
1041 |
8.2 |
7.5 |
26 |
1.17 |
4 |
Comp. ex. |
| 44 |
AC |
6678 |
46 |
999 |
43 |
92 |
987 |
4.6 |
11.1 |
25 |
0.47 |
3 |
Comp. ex. |
| 45 |
AD |
6346 |
41 |
1078 |
28 |
92 |
1045 |
2.8 |
5.3 |
14 |
1.00 |
3 |
Comp. ex. |
| Underlines indicate production conditions not preferable. |
[0065] The properties of the obtained steel sheets were measured and evaluated by the following
methods:
[Tensile Strength (TS)]
[0066] The tensile strength (TS) was measured by taking a JIS No. 5 test piece from an orientation(C
direction) where the longitudinal direction of the test piece became parallel with
a rolling perpendicular direction of each steel sheet and performing a tensile test
based on JIS Z 2241: 2011.
[Hole Expansion Rate (λ)]
[0067] The hole expansion rate was determined in the following way: First, a width 100 mm×length
100 mm test piece was taken from each steel sheet and a punch hole (initial hole:
hole diameter d0=10 mm) was prepared using a punch tool with a punch diameter of 10
mm and die diameter of 10.25 to 11.5 mm (clearance 12.5%). Next, while set so that
the burr became the die side, a 60° conical punch was used to expand the initial hole
until a crack passing through the sheet thickness was formed. The hole diameter d1mm
was measured at the time of cracking and the hole expansion rate λ (%) of each test
piece was found by the following formula. This hole expansion test was conducted three
times and the average value of the same was determined as the hole expansion rate
λ:

[Work Hardening Ability]
[0068] The work hardening ability was evaluated by finding the work hardening rate (WHR)
of steel sheetfrom a tensile test. Specifically, a state where the region where the
strain (true strain) during tensile deformation when performing a tensile test the
same as the case of measurement of TS became 0.04 or more was deemed as simulating
the state of the latter period of deformation in press-forming, and the maximum value
of the work hardening rate (WHR) in that region was found by the following formula:

where, σ is the true stress and ε is the true strain.
[0069] Cases where the tensile strength (TS) of the steel sheet was 980 MPa or more, the
hole expansion rate (λ) was 45% or more, and a maximum value of the work hardening
rate (WHR) in a region of true strain of 0.04 or more became 1000 MPa or more were
evaluated as steel sheet improved in hole expandability and work hardening ability
regardless of being high strength. The results are shown in Table 4.
[Table 4]
[0070]
Table 4
| Production no. |
Steel no |
Sheet thickness |
Microstructure |
Mechanical properties |
Remarks |
| Martensite |
Retained y |
Ferrite |
Bainite |
Pearlite |
Prior austenite grains |
Martensite |
TS |
λ |
Max. work hardening rate at true strain ≥0.04 |
| Mean particle size |
Area ratio of prior γ grains of aspect ratio 2.0 or less |
Area ratio of GOS≥4° crystal grains |
| mm |
Area% |
Area% |
Area% |
Area% |
Area% |
µm |
% |
% |
MPa |
% |
MPa |
| 1 |
A |
3.0 |
96.5 |
0.0 |
0.0 |
3.5 |
0.0 |
18.2 |
100.0 |
51.9 |
1176 |
76 |
1522 |
Inv. ex. |
| 2 |
A |
4.3 |
81.5 |
2.1 |
0.0 |
5.2 |
11.2 |
17.9 |
97.5 |
63.0 |
966 |
40 |
1118 |
Comp. ex. |
| 3 |
A |
4.0 |
92.8 |
2.2 |
0.0 |
5.0 |
0.0 |
33.6 |
88.0 |
51.5 |
1132 |
46 |
983 |
Comp. ex. |
| 4 |
A |
4.4 |
94.1 |
1.6 |
0.0 |
4.3 |
0.0 |
41.5 |
86.5 |
60.7 |
1188 |
48 |
952 |
Comp. ex. |
| 5 |
A |
2.7 |
94.4 |
1.7 |
0.0 |
3.9 |
0.0 |
44.1 |
96.6 |
60.2 |
1216 |
98 |
984 |
Comp. ex. |
| 6 |
A |
4.4 |
96.3 |
1.2 |
0.0 |
2.5 |
0.0 |
48.2 |
80.6 |
60.5 |
1153 |
48 |
996 |
Comp. ex. |
| 7 |
A |
3.2 |
96.4 |
1.0 |
0.0 |
2.6 |
0.0 |
60.8 |
76.3 |
64.4 |
1223 |
47 |
913 |
Comp. ex. |
| 8 |
A |
4.2 |
96.1 |
0.6 |
0.0 |
3.3 |
0.0 |
55.2 |
92.6 |
59.7 |
1133 |
74 |
882 |
Comp. ex. |
| 9 |
A |
3.8 |
96.5 |
0.8 |
0.0 |
2.7 |
0.0 |
31.3 |
88.2 |
53.9 |
1143 |
45 |
938 |
Comp. ex. |
| 10 |
A |
4.4 |
98.3 |
0.0 |
0.0 |
1.7 |
0.0 |
35.4 |
98.5 |
59.3 |
1256 |
100 |
891 |
Comp. ex. |
| 11 |
A |
3.1 |
83.0 |
0.1 |
10.8 |
3.8 |
2.3 |
25.4 |
93.5 |
53.9 |
953 |
38 |
1208 |
Comp. ex. |
| 12 |
A |
3.0 |
88.0 |
0.4 |
0.0 |
11.6 |
0.0 |
13.7 |
93.2 |
64.2 |
976 |
41 |
1096 |
Comp. ex. |
| 13 |
A |
3.6 |
96.0 |
2.3 |
0.0 |
1.7 |
0.0 |
22.7 |
96.3 |
44.2 |
1152 |
71 |
827 |
Comp. ex. |
| 14 |
A |
3.7 |
95.7 |
1.3 |
0.0 |
3.0 |
0.0 |
17.0 |
93.8 |
72.1 |
1048 |
92 |
776 |
Comp. ex. |
| 15 |
A |
3.8 |
95.4 |
0.1 |
0.0 |
4.5 |
0.0 |
13.7 |
91.6 |
42.7 |
1248 |
61 |
966 |
Comp. ex. |
| 16 |
A |
3.8 |
95.5 |
0.1 |
0.0 |
4.4 |
0.0 |
13.3 |
93.2 |
26.5 |
1211 |
89 |
853 |
Comp. ex. |
| 17 |
B |
2.8 |
95.4 |
0.4 |
0.0 |
4.2 |
0.0 |
19.3 |
95.0 |
58.0 |
1125 |
95 |
1519 |
Inv. ex. |
| 18 |
C |
1.4 |
93.6 |
1.8 |
0.0 |
4.6 |
0.0 |
25.2 |
91.8 |
52.0 |
1236 |
91 |
1081 |
Inv. ex. |
| 19 |
D |
2.8 |
94.2 |
2.8 |
0.0 |
3.0 |
0.0 |
19.2 |
97.5 |
57.7 |
1066 |
77 |
1502 |
Inv. ex. |
| 20 |
E |
3.0 |
94.5 |
0.8 |
0.0 |
4.7 |
0.0 |
13.2 |
95.7 |
60.0 |
1290 |
64 |
1675 |
Inv. ex. |
| 21 |
F |
4.2 |
94.8 |
0.2 |
0.0 |
5.0 |
0.0 |
20.7 |
91.9 |
60.8 |
1210 |
89 |
1126 |
Inv. ex. |
| 22 |
G |
6.6 |
90.1 |
0.2 |
9.6 |
0.1 |
0.0 |
16.1 |
92.8 |
56.1 |
982 |
49 |
1139 |
Inv. ex. |
| 23 |
H |
2.8 |
98.7 |
0.8 |
0.0 |
0.5 |
0.0 |
22.1 |
94.4 |
46.8 |
1169 |
53 |
1192 |
Inv. ex. |
| 24 |
I |
2.1 |
98.1 |
1.3 |
0.0 |
0.6 |
0.0 |
14.9 |
98.3 |
58.0 |
1073 |
69 |
1547 |
Inv. ex. |
| 25 |
J |
2.8 |
90.5 |
0.0 |
0.0 |
9.5 |
0.0 |
28.6 |
93.5 |
55.6 |
993 |
46 |
1015 |
Inv. ex. |
| 26 |
K |
3.7 |
98.0 |
0.8 |
0.0 |
1.2 |
0.0 |
23.6 |
98.0 |
51.5 |
1106 |
69 |
1453 |
Inv. ex. |
| 27 |
L |
4.2 |
98.0 |
0.9 |
0.0 |
1.1 |
0.0 |
18.8 |
98.7 |
64.7 |
1235 |
56 |
1205 |
Inv. ex. |
| 28 |
M |
3.5 |
98.6 |
0.2 |
0.0 |
1.2 |
0.0 |
15.8 |
94.6 |
59.0 |
1064 |
91 |
1256 |
Inv. ex. |
| 29 |
N |
2.5 |
95.9 |
1.0 |
0.0 |
3.1 |
0.0 |
17.9 |
96.3 |
53.1 |
1248 |
82 |
1472 |
Inv. ex. |
| 30 |
O |
3.6 |
93.9 |
1.8 |
0.0 |
4.3 |
0.0 |
21.4 |
100.0 |
59.9 |
1119 |
62 |
1643 |
Inv. ex. |
| 31 |
P |
3.8 |
94.6 |
1.0 |
0.0 |
4.4 |
0.0 |
15.6 |
95.5 |
61.1 |
1036 |
79 |
1523 |
Inv. ex. |
| 32 |
Q |
4.4 |
90.2 |
0.0 |
1.2 |
0.0 |
8.6 |
24.1 |
99.7 |
50.5 |
985 |
48 |
1395 |
Inv. ex. |
| 33 |
R |
7.6 |
96.8 |
0.8 |
0.0 |
2.4 |
0.0 |
19.1 |
99.1 |
56.2 |
1122 |
55 |
1305 |
Inv. ex. |
| 34 |
S |
3.1 |
97.4 |
2.3 |
0.0 |
0.3 |
0.0 |
18.2 |
95.2 |
68.8 |
1108 |
60 |
1657 |
Inv. ex. |
| 35 |
T |
2.5 |
96.7 |
1.2 |
0.0 |
2.1 |
0.0 |
22.1 |
99.8 |
65.0 |
1052 |
61 |
1394 |
Inv. ex. |
| 36 |
U |
4.3 |
98.1 |
1.4 |
0.0 |
0.5 |
0.0 |
25.5 |
93.8 |
60.5 |
1292 |
86 |
1248 |
Inv. ex. |
| 37 |
V |
4.4 |
99.0 |
0.4 |
0.0 |
0.6 |
0.0 |
20.1 |
92.7 |
63.0 |
926 |
92 |
1376 |
Comp. ex. |
| 38 |
W |
4.4 |
94.9 |
3.2 |
0.0 |
1.9 |
0.0 |
13.3 |
96.8 |
63.2 |
1244 |
33 |
1175 |
Comp. ex. |
| 39 |
X |
4.5 |
97.1 |
0.0 |
0.0 |
2.9 |
0.0 |
17.1 |
92.3 |
52.4 |
951 |
91 |
1550 |
Comp. ex. |
| 40 |
Y |
2.5 |
91.9 |
4.3 |
0.0 |
3.8 |
0.0 |
21.3 |
97.8 |
50.7 |
1188 |
36 |
1335 |
Comp. ex. |
| 41 |
Z |
3.3 |
87.7 |
0.6 |
2.2 |
8.3 |
1.2 |
14.3 |
98.8 |
61.6 |
950 |
67 |
1227 |
Comp. ex. |
| 42 |
AA |
2.8 |
92.7 |
2.4 |
0.0 |
4.9 |
0.0 |
14.7 |
93.2 |
56.2 |
1055 |
31 |
1372 |
Comp. ex. |
| 43 |
AB |
3.7 |
97.9 |
0.2 |
0.0 |
1.9 |
0.0 |
18.0 |
97.8 |
58.1 |
1238 |
38 |
1157 |
Comp. ex. |
| 44 |
AC |
3.2 |
95.6 |
2.1 |
0.0 |
2.3 |
0.0 |
41.9 |
98.5 |
51.0 |
1115 |
76 |
988 |
Comp. ex. |
| 45 |
AD |
3.3 |
94.1 |
1.9 |
0.0 |
4.0 |
0.0 |
19.8 |
99.1 |
54.4 |
1148 |
36 |
1481 |
Comp. ex. |
| Underlines indicate outside scope of present invention or not preferable properties. |
[0071] Referring to Tables 1 to 4, in Comparative Example 2, the holding time in the temperature
region of 1100°C or more in the heating step was short, and therefore it is believed
the coarse carbides incompletely dissolved and such carbides became starting points
for ferrite or bainite transformation, etc., in the subsequent cooling step. As a
result, the area ratio of martensite became less than 90.0% and the TS and λ fell.
In Comparative Examples 3 and 6, the respective rolling reductions in one stage before
the last stage and the last stage in the finish rolling were low, and therefore it
is believed recrystallization was not completed or was not sufficiently promoted.
As a result, the mean particle size of the prior austenite grains in the finally obtained
microstructure became larger and the work hardening ability of the steel sheet fell.
In Comparative Examples 4 and 7, the respective rolling temperature and final rolling
temperature in one stage before the last stage in the finish rolling were low, and
therefore it is believed recrystallization was not completed or was not sufficiently
promoted. As a result, the mean particle size of the prior austenite grains in the
finally obtained microstructure became larger and the work hardening ability of the
steel sheet fell. In Comparative Examples 5 and 8, the respective rolling temperature
and final rolling temperature in one stage before the last stage in the finish rolling
were high, and therefore it is believed the prior austenite grains became coarser
overall. As a result, the mean particle size of the prior austenite grains in the
finally obtained microstructure became larger and the work hardening ability of the
steel sheet fell. In Comparative Example 9, the time from the completion of the hot
rolling step to the start of the cooling step was short, and therefore it is believed
the recrystallization was not completed or was not sufficiently promoted. As a result,
the mean particle size of the prior austenite grains in the finally obtained microstructure
became larger and the work hardening ability of the steel sheet fell. In Comparative
Example 10, the time from the completion of the hot rolling step to the start of the
cooling step was long, and therefore it is believed the grain growth proceeded too
much overall. As a result, it was not possible to obtain the desired mean particle
size of the prior austenite grains and the work hardening ability of the steel sheet
fell. In Comparative Example 11, the time from the start of cooling to when becoming
400°C or less in the cooling step was long, and therefore the area ratio of martensite
became less than 90.0% and the TS and λ fell. In Comparative Example 12, the coiling
temperature was high, and therefore similarly the area ratio of martensite became
less than 90.0% and the TS and λ fell. In Comparative Example 13, the absolute value
of strain imparted in the strain imparting step was small, and therefore it is believed
dislocations were not sufficiently introduced in the crystal grains. As a result,
in the martensite, the ratio of crystal grains with an orientation difference in the
grains of 4° or more became smaller and the work hardening ability of the steel sheet
fell. In Comparative Example 14, the absolute value of strain imparted in the strain
imparting step was large, and therefore it is believed dislocations were excessively
accumulated in the crystal grains. As a result, in the martensite, the ratio of crystal
grains with an orientation difference in the grains of 4° or more became larger and
the work hardening ability of the steel sheet fell. In Comparative Example 15, the
number of times of imparting strain in the strain imparting step was small, and therefore
it is believed that dislocations were not sufficiently unevenly introduced inside
of the crystal grains. As a result, in the martensite, the ratio of crystal grains
with an orientation difference in the grains of 4° or more became smaller and the
work hardening ability of the steel sheet fell. In Comparative Example 16, the strain
imparting step was omitted, and therefore dislocations in the crystal grains could
not be unevenly introduced inside of the crystal grains. As a result, in the martensite,
the ratio of crystal grains with an orientation difference in the grains of 4° or
more became smaller and the work hardening ability of the steel sheet fell.
[0072] In Comparative Examples 37 and 39, the respective C and Si contents were low, and
therefore the TS fell. On the other hand, in Comparative Example 38 and in Comparative
Example 40, the respective C and Si contents were high, and therefore the retained
austenite was formed in a relatively large amount and the λ fell. In Comparative Example
41, the Mn content was low, and therefore the hardenability fell and as a result the
area ratio of martensite became lower and the TS fell. In Comparative Example 42,
the Mn content was high, and therefore the λ fell. In Comparative Example 43, the
sol. Al content was low, and therefore it is believed precipitation of cementite could
not be sufficiently suppressed. As a result, the λ fell. In Comparative Example 44,
the Nb content was low, and therefore it is believed refinement of the prior austenite
grains due to the pinning effect could not be sufficiently promoted. As a result,
the mean particle size of the prior austenite grains in the finally obtained microstructure
became larger and the work hardening ability of the steel sheet fell. In Comparative
Example 45, the Nb content was high, and therefore it is believed coarse carbides,
etc., formed in the steel. As a result, the λ fell.
[0073] In contrast to this, in the steel sheets according to all of the invention examples,
by having a predetermined chemical composition and, furthermore, by suitably controlling
the conditions in the method of production, it was possible to obtain steel sheet
having a microstructure containing an area% of martensite: 90.0% or more and retained
austenite: 3.0% or less, having a mean particle size of prior austenite grains of
30.0 µm or less, and having in the martensite a ratio of crystal grains with an orientation
difference in the grains of 4° or more of an area% of 45.0 to 70.0%. Further, as a
result, regardless of being a high strength of a tensile strength of 980 MPa or more,
it was possible to remarkably improve the hole expandability and work hardening ability.