Technical Field
[0001] The present invention relates to a thin steel sheet for automobile use excellent
in notch-fatigue strength, and a method for producing the steel sheet, and, more specifically,
to a thin steel sheet for automobile use excellent in notch-fatigue strength and suitable
as the material for undercarriage components of an automobile and the like to overcome
the problem of the propagation of a fatigue crack from a site of stress concentration
such as a blanked or welded portion, and a method for producing the steel sheet.
Background Art
[0002] The application of light metals such as aluminum alloys and high-strength steel sheets
to automobile members has expanded recently for the purposes of reducing automobile
weight and thereby reducing the fuel consumption and the like. However, while light
metals such as aluminum alloys have an advantage of high specific strength, their
application is limited to special uses because they are far more costly than steel.
For further reducing the automobile weight, therefore, a wider application of low-cost
high-strength steel sheets is required.
[0003] In response to the requirement for such high-strength steel materials, in the field
of cold-rolled steel sheets used for a white body and panels which account for about
one fourth of the weight of an automobile, a steel sheet having both high strength
and deep drawability, a steel sheet having bake-hardenability and the like, have so
far been developed and have contributed to the weight reduction of an automobile body.
However, the focus of the efforts for reducing the weight of an automobile has shifted
lately to structural and undercarriage members which account for roughly 20% of the
automobile body weight. As a consequence, the development of a high-strength steel
sheet applicable to those members has come to be required as a matter of urgency.
[0004] However, as the strengthening of a steel material usually leads to the deterioration
of formability (workability) and so on, a key issue in the development of a high-strength
steel sheet for those applications is how to realize a high strength without sacrificing
those material properties. The important properties required especially of a steel
sheet for the structural and undercarriage members of an automobile include shearing
and blanking workability, burring workability, fatigue resistance, corrosion resistance
and so forth, not to mention elongation; it is essential to balance a high strength
with these properties at high levels.
[0005] For instance, an undercarriage component such as a suspension arm is produced through
the processes of blanking and boring by shearing and punching, thereafter press forming
and, in some cases, welding. It is often the case with such a component that a crack
propagates from a point near a sheared end face or a weld and causes fatigue fracture.
In other words, a sheared end face or a weld acts as a stress concentration site like
a notch and a fatigue crack propagates therefrom.
[0006] Meanwhile, in general, the fatigue limit of a material is lowered as a notch becomes
acute. When the acuteness of a notch surpasses a certain extent, however, a fatigue
limit does not lower any further. This is because a fatigue limit shifts from being
dominated by a crack initiation limit toward being dominated by a crack propagation
limit as the acuteness of a notch increases. When the strength of a material increases,
while a crack initiation limit increases, a crack propagation limit does not, and
therefore the acuteness of a notch, at which a fatigue limit shifts from being dominated
by a crack initiation limit toward being dominated by a crack propagation limit, moves
toward an acuter side. As a result, when a material has an acute notch, even if the
strength of the material is increased, the decrease in the fatigue limit resulting
from the acuteness of the notch becomes significant and thus the advantages of the
high strength are not secured. In other words, when the strength of a material is
increased, the sensitivity thereof to a notch increases.
[0007] Thin steel sheets having strength of the 340 to 440 MPa class are presently used
for the undercarriage members of an automobile. However, the level of strength required
of the steel sheets for those members is rising toward the 590 to 780 MPa class. Therefore,
to satisfactorily respond to such a requirement, it is essential to develop a steel
sheet with which the advantages of high strength can be secured even when an acute
notch exists.
[0008] There are basically two methods for enhancing the fatigue strength of a steel sheet
having an end face formed by blanking or shearing: one is to remove an acute notch
such as a burr formed at a blanking or shearing end face, and the other is to enhance
the resistance to the propagation of a crack even when such an acute notch exists.
[0009] There are the following methods as examples of inventions based on the former method.
Japanese Unexamined Patent Publication No. H5-51695 discloses a technology wherein
the occurrence of a burr is suppressed by reducing the addition amount of Si and forming
precipitates of Ti, Nb and V for lowering breaking elongation and thereby the fatigue
strength of an as-blanked or as-sheared steel sheet is enhanced. Japanese Unexamined
Patent Publication No. H5-179346 discloses a technology wherein the upper limit of
the volume percentage of bainite is regulated by defining an upper limit of a finish
rolling temperature and, thereby, the fatigue strength of an as-blanked or as-sheared
steel sheet is enhanced. Japanese Unexamined Patent Publication No. H8-13033 discloses
a technology wherein the formation of martensite is suppressed by defining a cooling
rate after rolling and, thereby, the fatigue strength of an as-blanked or as-sheared
steel sheet is enhanced.
[0010] Further, Japanese Unexamined Patent Publication No. H8-302446 discloses a technology
wherein strain energy during blanking or shearing is reduced by regulating the hardness
of the second phase of a dual phase steel to at least 1.3 times that of ferrite and,
thereby, the fatigue strength of an as-blanked or as-sheared steel sheet is enhanced.
Japanese Unexamined Patent Publication No. H9-170048 discloses a technology wherein
the occurrence of a burr during blanking or shearing is suppressed by regulating the
length of intergranular cementite and thereby the fatigue strength of an as-blanked
or as-sheared steel sheet is enhanced. Furthermore, Japanese Unexamined Patent Publication
No. H9-202940 discloses a technology wherein blanking performance is improved by regulating
a parameter based on the addition amounts of Ti, Nb and Cr and thereby the fatigue
strength of an as-blanked steel sheet is enhanced.
[0011] Meanwhile, there are the following methods as the examples of the inventions based
on the latter method. Japanese Unexamined Patent Publication No. H6-88161 discloses
a technology wherein the X-ray diffraction strength ratio of a (100) plane parallel
to the rolling surfaces in the texture at a steel sheet surface layer is regulated
to 1.5 or more and, thereby, a fatigue crack propagation speed is lowered. Further,
Japanese Unexamined Patent Publications No. H8-199286 and No. H10-147846 disclose
technologies wherein the area percentage of recovered or recrystallized ferrite is
controlled in the range from 15 to 40% by regulating the X-ray diffraction strength
ratio of a (200) plane in the thickness direction in the range from 2.0 to 15.0 and,
thereby, a fatigue crack propagation speed is lowered.
[0012] However, in the cases of the technologies of suppressing an acute notch such as a
burr generated at a blanked or sheared end face as disclosed in the above Japanese
Unexamined Patent Publications No. H5-51695, No. H5-179346, No. H8-13033, No. H8-302446,
No. H9-170048, No. H9-202940 and so forth, as the degree of a generated burr largely
varies with the clearance of tools at blanking or shearing, the technologies are not
ones that can be employed under any conditions. Therefore, it must be said that the
technologies are insufficient when be applied to a steel sheet excellent in notch-fatigue
strength.
[0013] On the other hand, technologies of enhancing the resistance to crack propagation
by controlling the texture of a steel sheet as disclosed in the above Japanese Unexamined
Patent Publications No. H6-88161, No. H8-199286 and No. H10-147846 are the inventions
mainly intended for steels used for large structures such as construction machines,
ships and bridges and are not intended for a thin steel sheet, used for automobiles,
for which the present invention is intended.
[0014] In addition, the aforementioned technologies are ones wherein a fatigue crack propagation
speed is controlled in a PARIS zone that is referred to in the fracture mechanics
of a fatigue crack mainly propagating from a weld toe portion and therefore are insufficient
as technologies to be employed in such a case as a thin steel sheet, for automobile
use, where a crack propagation zone is not included in the PARIS zone because of the
thickness of the steel sheet.
[0015] Besides the above, no invention has been proposed up to now wherein notch-fatigue
properties are evaluated using a test piece, as shown in Fig. 1(b), in a plane bending
fatigue test method applied to a thin steel sheet.
Disclosure of the Invention
[0016] In view of the above situation, the present invention relates to a technology wherein
the notch-fatigue strength of a thin steel sheet for automobile use is improved by
controlling the texture of the steel sheet and thus enhancing the resistance to a
fatigue crack propagating from a notch such as an end face formed after blanking or
shearing, regardless of the conditions such as the clearance of tools during blanking
or shearing. In other words, the object of the present invention is to provide a thin
steel sheet for automobile use excellent in notch-fatigue strength and a method for
producing the steel sheet economically and stably.
[0017] The present inventors, in consideration of the production processes of thin steel
sheets presently produced on an industrial scale using generally employed production
facilities, earnestly studied methods for enhancing the notch-fatigue strength of
a thin steel sheet for automobile use. As a result, the present invention has been
established on the basis of a new discovery that the following conditions are very
effective for enhancing notch-fatigue strength: that, on a plane at an arbitrary depth
within 0.5 mm from the surface of a steel sheet in the thickness direction thereof,
the average of the ratios of the X-ray diffraction strength in the orientation component
group of {100}<011> to {223}<110> to random X-ray diffraction strength is 2 or more
and the average of the ratios of the X-ray diffraction strength in the three orientation
components of {554}<225>, {111}<112> and <111}<110> to random X-ray diffraction strength
is 4 or less; and that the thickness of the steel sheet is in the range from 0.5 to
12 mm.
[0018] The gist of the present invention, therefore, is as follows:
(1) A thin steel sheet for automobile use excellent in notch-fatigue strength, characterized
in: that, on a plane at an arbitrary depth within 0.5 mm from the surface of the steel
sheet in the thickness direction thereof, the average of the ratios of the X-ray diffraction
strength in the orientation component group of {100}<011> to {223}<110> to random
X-ray diffraction strength is 2 or more and the average of the ratios of the X-ray
diffraction strength in the three orientation components of {554}<225>, {111}<112>
and {111}<110> to random X-ray diffraction strength is 4 or less; and that the thickness
of the steel sheet is in the range from 0.5 to 12 mm.
(2) A thin steel sheet for automobile use excellent in notch-fatigue strength according
to the item (1), characterized in that the microstructure of the steel sheet is a
compound structure containing bainite or ferrite and bainite as the phase accounting
for the largest volume percentage.
(3) A thin steel sheet for automobile use excellent in notch-fatigue strength according
to the item (1), characterized in that the microstructure of the steel sheet is a
compound structure containing retained austenite by 5 to 25% in terms of volume percentage
and having the balance mainly consisting of ferrite and bainite.
(4) A thin steel sheet for automobile use excellent in notch-fatigue strength according
to the item (1), characterized in that the microstructure of the steel sheet is a
compound structure containing ferrite as the phase accounting for the largest volume
percentage and martensite as the second phase.
(5) A thin steel sheet for automobile use excellent in notch-fatigue strength, the
steel sheet containing, in mass, 0.01 to 0.3% C, 0.01 to 2% Si, 0.05 to 3% Mn, 0.1%
or less P, 0.01% or less S and 0.005 to 1% Al, with the balance consisting of Fe and
unavoidable impurities, characterized in: that, on a plane at an arbitrary depth within
0.5 mm from the surface of the steel sheet in the thickness direction thereof, the
average of the ratios of the X-ray diffraction strength in the orientation component
group of {100}<011> to {223}<110> to random X-ray diffraction strength is 2 or more
and the average of the ratios of the X-ray diffraction strength in the three orientation
components of {554}<225>, {111} <112> and {111}<110> to random X-ray diffraction strength
is 4 or less; and that the thickness of the steel sheet is in the range from 0.5 to
12 mm.
(6) A thin steel sheet for automobile use excellent in notch-fatigue strength according
to the item (5), characterized by further containing, in mass, one or more of 0.2
to 2% Cu, 0.0002 to 0.002% B, 0.1 to 1% Ni, 0.0005 to 0.002% Ca, 0.0005 to 0.02% REM,
0.05 to 0.5% Ti, 0.01 to 0.5% Nb, 0.05 to 1% Mo, 0.02 to 0.2% V, 0.01 to 1% Cr and
0.02 to 0.2% Zr.
(7) A thin steel sheet for automobile use excellent in notch-fatigue strength according
to the item (5) or (6), characterized in that the microstructure of the steel sheet
is any one of 1) a compound structure containing bainite or ferrite and bainite as
the phase accounting for the largest volume percentage, 2) a compound structure containing
retained austenite by 5 to 25% in terms of volume percentage and having the balance
mainly consisting of ferrite and bainite, and 3) a compound structure containing ferrite
as the phase accounting for the largest volume percentage and martensite as the second
phase.
(8) A thin steel sheet for automobile use excellent in notch-fatigue strength, characterized
in that the steel sheet is produced by applying galvanizing to a thin steel sheet
for automobile use according to any one of the items (1) to (7).
(9) A method for producing a thin steel sheet for automobile use excellent in notch-fatigue
strength characterized in: that a steel slab containing, in mass, 0.01 to 0.3% C,
0.01 to 2% Si, 0.05 to 3% Mn, 0.1% or less P, 0.01% or less S and 0.005 to 1% Al,
with the balance consisting of Fe and unavoidable impurities, is subjected, in a hot
rolling process, to rough rolling and then to finish rolling at a total reduction
ratio of 25% or more in terms of steel sheet thickness in the temperature range of
the Ar3 transformation temperature + 100°C or lower; that, on a plane at an arbitrary depth
within 0.5 mm from the surface of the steel sheet in the thickness direction thereof,
the average of the ratios of the X-ray diffraction strength in the orientation component
group of {100}<011> to {223}<110> to random X-ray diffraction strength is 2 or more
and the average of the ratios of the X-ray diffraction strength in the three orientation
components of {554}<225>, {111}<112> and {111}<110> to random X-ray diffraction strength
is 4 or less; and that the thickness of the steel sheet is in the range from 0.5 to
12 mm.
(10) A method for producing a thin steel sheet for automobile use excellent in notch-fatigue
strength according to the item (9), characterized by: cooling the steel sheet at a
cooling rate of 20°C/sec. or higher after the finish rolling; and then coiling it
at a coiling temperature of 450°C or higher.
(11) A method for producing a thin steel sheet for automobile use excellent in notch-fatigue
strength according to the item (9), characterized by: retaining the steel sheet for
1 to 20 sec. in the temperature range from the Ar1 transformation temperature to the Ar3 transformation temperature after the finish rolling; then cooling it at a cooling
rate of 20°C/sec. or higher; and coiling it at a coiling temperature in the range
from higher than 350°C to lower than 450°C.
(12) A method for producing a thin steel sheet for automobile use excellent in notch-fatigue
strength according to the item (11), characterized by coiling the steel sheet at a
coiling temperature of 350°C or lower after the cooling.
(13) A method for producing a thin steel sheet for automobile use excellent in notch-fatigue
strength according to any one of the items (9) to (12), characterized by applying
lubrication rolling to the steel sheet in the hot rolling.
(14) A method for producing a thin steel sheet for automobile use excellent in notch-fatigue
strength according to any one of the items (9) to (13), characterized by applying
descaling to the steel sheet after the completion of the rough rolling in the hot
rolling.
(15) A method for producing a thin steel sheet for automobile use excellent in notch-fatigue
strength, characterized in: that a steel slab containing, in mass, 0.01 to 0.3% C,
0.01 to 2% Si, 0.05 to 3% Mn, 0.1% or less P, 0.01% or less S and 0.005 to 1% Al,
with the balance consisting of Fe and unavoidable impurities, is subjected to rough
rolling, then finish rolling at a total reduction ratio of 25% or more in terms of
steel sheet thickness in the temperature range of the Ar3 transformation temperature + 100°C or lower, pickling, cold rolling at a reduction
ratio of less than 80% in terms of steel sheet thickness, and then annealing for recovery
or recrystallization comprising the processes of retaining the cold-rolled steel sheet
for 5 to 150 sec. in the temperature range from the recovering temperature to the
Ac3 transformation temperature + 100°C and then cooling it; that, on a plane at an arbitrary
depth within 0.5 mm from the surface of the steel sheet in the thickness direction
thereof, the average of the ratios of the X-ray diffraction strength in the orientation
component group of {100}<011> to {223}<110> to random X-ray diffraction strength is
2 or more and the average of the ratios of the X-ray diffraction strength in the three
orientation components of {554}<225>, {111}<112> and {111}<110> to random X-ray diffraction
strength is 4 or less; and that the thickness of the steel sheet is in the range from
0.5 to 12 mm.
(16) A method for producing a thin steel sheet for automobile use excellent in notch-fatigue
strength according to the item (15), characterized by subjecting the steel sheet after
the cold rolling to a heat treatment comprising the processes of retaining the cold-rolled
steel sheet for 5 to 150 sec. in the temperature range from the Ac1 transformation temperature to the Ac3 transformation temperature + 100°C and then cooling it.
(17) A method for producing a thin steel sheet for automobile use excellent in notch-fatigue
strength according to the item (15), characterized by subjecting the steel sheet to
a heat treatment comprising the processes of, in sequence, retaining the cold-rolled
steel sheet for 5 to 150 sec. in said temperature range, cooling it at a cooling rate
of 20°C/sec. or higher to the temperature range from higher than 350°C to lower than
450°C, retaining it for 5 to 600 sec. in said temperature range, and then cooling
it at a cooling rate of 5°C/sec. or higher to the temperature range of 200°C or lower.
(18) A method for producing a thin steel sheet for automobile use excellent in notch-fatigue
strength according to the item (15), characterized by subjecting the steel sheet to
a heat treatment comprising the processes of retaining the cold-rolled steel sheet
for 5 to 150 sec. in said temperature range and then cooling it at a cooling rate
of 20°C/sec. or higher to the temperature range of 350°C or lower.
(19) A method for producing a thin steel sheet for automobile use excellent in notch-fatigue
strength, characterized in that the steel sheet produced by the method according to
any one of the items (11) to (18) further contains, in mass, one or more of 0.2 to
2% Cu, 0.0002 to 0.002% B, 0.1 to 1% Ni, 0.0005 to 0.002% Ca, 0.0005 to 0.02% REM,
0.05 to 0.5% Ti, 0.01 to 0.5% Nb, 0.05 to 1% Mo, 0.02 to 0.2% V, 0.01 to 1% Cr and
0.02 to 0.2% Zr.
(20) A method for producing a thin steel sheet for automobile use excellent in notch-fatigue
strength according to the item (10) or (16), characterized in that the microstructure
of the steel sheet is a compound structure containing bainite or ferrite and bainite
as the phase accounting for the largest volume percentage.
(21) A method for producing a thin steel sheet for automobile use excellent in notch-fatigue
strength according to the item (11) or (17), characterized in that the microstructure
of the steel sheet is a compound structure containing retained austenite at 5 to 25%
in terms of volume percentage and having the balance mainly consisting of ferrite
and bainite.
(22) A method for producing a thin steel sheet for automobile use excellent in notch-fatigue
strength according to the item (12) or (18), characterized in that the microstructure
of the steel sheet is a compound structure containing ferrite as the phase accounting
for the largest volume percentage and martensite as the second phase.
(23) A method for producing a thin steel sheet for automobile use excellent in notch-fatigue
strength characterized by, after producing a hot-rolled steel sheet or a steel sheet
annealed for recovery or recrystallization according to any one of the items (9) to
(22), further applying galvanizing to the surfaces of the steel sheet by dipping the
steel sheet in a zinc plating both.
(24) A method for producing a thin steel sheet for automobile use excellent in notch-fatigue
strength according to the item (23), characterized by subjecting the steel sheet further
to an alloying treatment after the galvanizing.
Brief Description of the Drawings
[0019]
Fig. 1 consists of illustrations showing the shapes of test pieces for fatigue test:
Fig. 1(a) shows an unnotched test piece for fatigue test, and Fig. 1(b) a notched
test piece for fatigue test.
Fig. 2 is a graph showing the result of a preliminary test that leads to the present
invention in terms of the relationship among: the average of the ratios of the X-ray
diffraction strength in the orientation component group of {100}<011> to {223}<110>
to random X-ray diffraction strength; the average of the ratios of the X-ray diffraction
strength in the three orientation components of {554}<225>, {111}<112> and {111}<110>
to random X-ray diffraction strength; and notch-fatigue strength (the fatigue strength
for finite life after 107 cycles of repetition, namely the fatigue limit).
Best Mode for Carrying out the Invention
[0020] In the first place, the results of preliminary studies that lead to the present invention
are explained hereafter.
[0021] Generally speaking, a fatigue crack of a steel sheet starts from the surface thereof;
this is true also with the case where a stress concentration site such as a notch
exists. In the case where an end face formed by blanking or shearing exists, it is
often observed that, under a repeated load including a loading mode in the out-of-plane
bending direction, a fatigue crack starts and propagates from an end of a steel sheet
surface. It is clear from this that, even in such a case, it is effective for enhancing
notch-fatigue strength to increase resistance to crack propagation at the surface
of a steel sheet or in the layer from the surface to a depth of several crystal grains
or so. On the other hand, even though resistance to crack propagation is increased
at the thickness center of a steel sheet, it is difficult to arrest an already formed
crack. For this reason, in the present invention, the range of a steel sheet texture
effective in enhancing fatigue strength is limited to the range from the surface to
a depth of 0.5 mm in the thickness direction. The range is, more adequately, to a
depth of 0.1 mm.
[0022] The present inventors investigated the influences of the average of the ratios of
the X-ray diffraction strength in the orientation component group of {100}<011> to
{223}<110> to random X-ray diffraction strength and the average of the ratios of the
X-ray diffraction strength in the three orientation components of {554}<225>, {111}<112>
and {111}<110> to random X-ray diffraction strength on a plane at an arbitrary depth
in the range from the surface of a steel sheet to a depth of 0.5 mm in the thickness
direction thereof over notch-fatigue strength. The specimens for the investigation
were prepared by melting a steel and adjusting the chemical components thereof so
that the steel contained 0.08% C, 0.9% Si, 1.2% Mn, 0.01% P, 0.001% S, and 0.03% Al,
casting it into a slab, hot rolling the slab to a thickness of 3.5 mm so that the
finish rolling was completed at a temperature of not lower than the Ar
3 transformation temperature, and then coiling the hot-rolled steel sheet.
[0023] For the purpose of measuring the average of the ratios of the X-ray diffraction strength
in the orientation component group of {100}<011> to {223}<110> to random X-ray diffraction
strength and the average of the ratios of the X-ray diffraction strength in the three
orientation components of {554}<225>, {111}<112> and {111}<110> to random X-ray diffraction
strength on a plane at an arbitrary depth within 0.5 mm from the surface of a steel
sheet obtained as above in the thickness direction thereof, a test piece was prepared
by cutting out a specimen sheet 30 mm in diameter from a position of 1/4 or 3/4 of
the width of a steel sheet, grinding the surface of the specimen sheet to a depth
of about 0.05 mm from the surface so that the surface might have the second finest
finish, and then removing strain by chemical polishing or electrolytic polishing.
[0024] Note that a crystal orientation component expressed as {hkl}<uvw> means that the
direction of a normal to the plane of a steel sheet is parallel to <hkl> and the rolling
direction of the steel sheet is parallel to <uvw>. The measurement of a crystal orientation
with X-rays is conducted, for example, in accordance with the method described in
pages 274 to 296 of the Japanese translation of Elements of X-ray Diffraction by B.
D. Cullity (published in 1986 by AGNE Gijutsu Center, translated by Gentaro Matsumura).
[0025] Here, the average of the ratios of the X-ray diffraction strength in the orientation
component group of {100}<011> to {223}<110> to random X-ray diffraction strength is
obtained from the X-ray diffraction strengths in the principal orientation components
included in said orientation component group, namely {100}<011>, {116}<110>, {114}<110>,
{113}<110>, {112}<110>, {335}<110> and {223}<110>, in the three-dimensional texture
calculated either by the vector method based on the pole figure of {110} or by the
series expansion method using two or more (desirably, three or more) pole figures
out of the pole figures of {110}, {100}, {211} and {310}.
[0026] For example, in the case of obtaining the ratios of the X-ray diffraction strength
in the above crystal orientation components to random X-ray diffraction strength by
the latter method, the strengths of (001)[1-10], (116) [1-10), (114)[1-10], (113)[1-10],
(112)[1-10], (335)[1-10] and (223) [1-10] at a φ2 = 45° cross section in a three-dimensional
texture may be used without modification. Note that the average of the ratios of the
X-ray diffraction strength in the orientation component group of {100}<011> to {223}<110>
to random X-ray diffraction strength is the arithmetic average of the ratios in all
the above orientation components.
[0027] When it is impossible to obtain the strengths in all these orientation components,
the arithmetic average of the strengths in the orientation components of {100}<011>,
{116}<110>, {114}<110>, {112}<110> and {223}<110> may be used as a substitute.
[0028] Likewise, the average of the ratios of the X-ray diffraction strength in the three
orientation components of {554}<225>, {111}<112> and {111}<110> to random X-ray diffraction
strength can be obtained from the three-dimensional texture calculated in the same
manner as explained above.
[0029] Next, for the purpose of investigating the notch-fatigue strength of the above steel
sheet, a test piece for fatigue test having the shape shown in Fig. 1(b) was cut out
from a position of 1/4 or 3/4 of the width of the steel sheet so that the longitudinal
direction of the test piece coincided with the rolling direction of the steel sheet,
and was subjected to a fatigue test. It has to be noted here that, whereas a test
piece for fatigue test shown in Fig. 1(a) is a common unnotched test piece for evaluating
the fatigue strength of a steel material, a test piece for fatigue test shown in Fig.
1(b) is a notched test piece prepared for evaluating notch-fatigue strength. A test
piece for fatigue test was ground to a depth of about 0.05 mm from the surface so
that the surface might have the second finest finish, and a fatigue test was carried
out using an electro-hydraulic servo type fatigue tester and the methods conforming
to JIS Z 2273-1978 and JIS Z 2275-1978.
[0030] Fig. 2 shows the results of an investigation of the influences of the average of
the ratios of the X-ray diffraction strength in the orientation component group of
{100}<011> to {223}<110> to random X-ray diffraction strength and the average of the
ratios of the X-ray diffraction strength in the three orientation components of {554}<225>,
{111}<112> and {111}<110> to random X-ray diffraction strength over notch-fatigue
strength. The numeral in a circle in the figure indicates the fatigue limit (the fatigue
strength for finite life after 10
7 cycles of repetition) obtained through a fatigue test using a notched test piece
having the shape shown in Fig. 1(b); the numeral is hereinafter referred to as a notch-fatigue
strength.
[0031] It has been clarified that there is a strong correlation among: the average of the
ratios of the X-ray diffraction strength in the orientation component group of {100}<011>
to {223}<110> to random X-ray diffraction strength; the average of the ratios of the
X-ray diffraction strength in the three orientation components of {554}<225>, {111}<112>
and {111}<110> to random X-ray diffraction strength; and notch-fatigue strength, and
that notch-fatigue strength is remarkably enhanced when the above average figures
are 2 or more and 4 or less, respectively.
[0032] As a result of closely examining the results of those tests, the present inventors
have newly found that it is very important, for enhancing notch-fatigue strength,
that, on a plane at an arbitrary depth within 0.5 mm from the surface of a steel sheet
in the thickness direction thereof, the average of the ratios of the X-ray diffraction
strength in the orientation component group of {100}<011> to {223}<110> to random
X-ray diffraction strength is 2 or more and the average of the ratios of the X-ray
diffraction strength in the three orientation components of {554}<225>, {111}<112>
and {111}<110> to random X-ray diffraction strength is 4 or less.
[0033] Further, for enhancing the resistance to the occurrence of a fatigue crack not only
in a notched test piece but also in an unnotched test piece, it is desirable that,
on a plane at an arbitrary depth within 0.5 mm from the surface of a steel sheet in
the thickness direction thereof, the average of the ratios of the X-ray diffraction
strength in the orientation component group of {100}<011> to {223}<110> to random
X-ray diffraction strength is 4 or more and the average of the ratios of the X-ray
diffraction strength in the three orientation components of {554}<225>, {111}<112>
and {111} <110> to random X-ray diffraction strength is 2.5 or less.
[0034] The reason for the above is not altogether clear, but it is presumed to be as follows.
[0035] Generally speaking, in the case where an acute notch exists, the fatigue limit of
a material is determined by the crack propagation limit of the material, namely the
degree of the resistance to the propagation of a crack for arresting the crack. The
propagation of a fatigue crack is caused by the repetition of small plastic deformation
at the bottom of a notch or a stress concentration site, and it is presumed that,
when a crack length is comparatively small and plastic deformation occurs within a
range comparable to the size of a crystal grain, the crack propagation is significantly
influenced by crystallographic slip planes and slip directions. Therefore, if the
proportion of the crystal grains having slip planes and slip directions that show
a high resistance to crack propagation is large in the crack propagation direction
and on the plane of a crack, then the propagation of the fatigue crack is suppressed.
[0036] Next, the reasons for limiting the thickness of a steel sheet in the present invention
are explained.
[0037] When the thickness of a steel sheet is less than 0.5 mm, the conditions of allowing
the occurrence of a small-scale yield are not satisfied regardless of the extent of
stress concentration and therefore there is a danger that monotonic ductile fracture
is caused. In addition, as the sufficient constraint of plastic deformation is required
from the viewpoint of arresting a crack, it is desirable that the thickness of a steel
sheet is 1.2 mm or more for maintaining the state of plane strain.
[0038] When the thickness of a steel sheet exceeds 12 mm, on the other hand, the deterioration
of fatigue strength resulting from thickness effect (size effect) becomes significant.
Further, when the thickness of a steel sheet exceeds 8 mm, an excessive load may be
required to be imposed on production facilities for achieving the conditions of hot
or cold rolling that allow a texture effective for enhancing notch-fatigue strength
to be obtained. For that reason, a desirable thickness is 8 mm or less. As a conclusion,
the thickness of a steel sheet is limited to 0.5 to 12 mm, or desirably 1.2 to 8 mm,
in the present invention.
[0039] The microstructure of a steel sheet according to the present invention is explained
hereafter.
[0040] In the present invention, it is not necessary to specify the microstructure of a
steel sheet for the purpose of enhancing the notch-fatigue strength of the steel sheet.
The effect of enhancing notch-fatigue strength in the present invention is obtained
as far as a texture falls in the range specified in the present invention (a texture
showing the ratios of the X-ray diffraction strength in specific orientation components
to random X-ray diffraction strength falling in the ranges specified in the present
invention) in the structures of ferrite, bainite, pearlite and martensite forming
in a commonly used steel material. Therefore, it is desirable to regulate the microstructure
of a steel sheet in consideration of other required material properties. It has to
be noted, however, that the above effect is further enhanced when a microstructure
is a specific microstructure, for example, a compound structure containing retained
austenite by 5 to 25% in terms of volume percentage and having the balance mainly
consisting of ferrite and bainite, a compound structure containing ferrite as the
phase accounting for the largest volume percentage and mainly martensite as the second
phase, or the like.
[0041] Note that the ferrite mentioned here includes bainitic ferrite and acicular ferrite.
Note also that, when a structure which is not a bcc crystal structure, such as retained
austenite, is included in a compound structure composed of two or more phases, such
a compound structure does not pose any problem insofar as the ratios of the X-ray
diffraction strength in the orientation components and orientation component groups
to random X-ray diffraction strength converted by the volume percentage of the other
structures are within the relevant ranges according to the present invention. Besides,
as pearlite containing coarse carbides may act as a starting point of a fatigue crack
and remarkably deteriorate fatigue strength, it is desirable that the volume percentage
of the pearlite containing coarse carbides is 15% or less. When still better fatigue
properties are required, it is desirable that the volume percentage of the pearlite
containing coarse carbides is 5% or less.
[0042] Here, the volume percentage of ferrite, bainite, pearlite, martensite or retained
austenite is defined as the area percentage thereof in a microstructure observed with
an optical microscope under a magnification of 200 to 500 at a position in the depth
of 1/4 of the steel sheet thickness on a section surface along the rolling direction
of a specimen which is cut out from a position of 1/4 or 3/4 of the width of the steel
sheet, the section surface being polished and etched with a nitral reagent and/or
the reagent disclosed in Japanese Unexamined Patent Publication No. H5-163590. As
it is sometimes difficult to identify retained austenite by the etching with the above
reagents, the volume percentage may also be calculated in the following manner.
[0043] Because the crystal structure of austenite is different from that of ferrite, they
can be easily distinguished from each other crystallographically. Therefore, the volume
percentage of retained austenite can be obtained experimentally by the X-ray diffraction
method too, namely by the simplified method wherein the volume percentage thereof
is calculated with the following equation on the basis of the difference between austenite
and ferrite in the reflection intensity of the Kα ray of Mo on their lattice planes:

where, α(211), γ(220) and γ(311) are the X-ray reflection intensities of the indicated
lattice planes of ferrite (α) and austenite (γ), respectively.
[0044] For the purpose of obtaining a good burring workability in addition to enhancing
notch-fatigue strength in the present invention, it is necessary that the microstructure
of a steel sheet is a compound structure containing bainite or ferrite and bainite
as the phase accounting for the largest volume percentage. Here, in this case, the
present invention allows the compound structure to contain unavoidably included martensite,
retained austenite and pearlite. For the purpose of obtaining a good burring workability
(a hole expansion ratio), it is desirable that the total volume percentage of hard
retained austenite and martensite is less than 5%. It is also desirable that the volume
percentage of bainite is 30% or more. Further, for realizing a good ductility, it
is desirable that the volume percentage of bainite is 70% or less.
[0045] Further, for the purpose of obtaining a good ductility in addition to enhancing notch-fatigue
strength in the present invention, it is necessary that the microstructure of a steel
sheet is a compound structure containing retained austenite by 5 to 25% in terms of
volume percentage and having the balance mainly consisting of ferrite and bainite.
Here, in this case, the present invention allows the compound structure to contain
unavoidably included martensite and pearlite as far as their total volume percentage
is less than 5%.
[0046] Furthermore, for the purpose of obtaining a low yield ratio for realizing a good
shape-fixation property in addition to enhancing notch-fatigue strength in the present
invention, it is necessary that the microstructure of a steel sheet is a compound
structure containing ferrite as the phase accounting for the largest volume percentage
and mainly martensite as the second phase. Here, in this case, the present invention
allows the compound structure to contain unavoidably included bainite, retained austenite
and pearlite as far as their total volume percentage is less than 5%. Note that, for
securing a low yield ratio of 70% or less, it is desirable that the volume percentage
of ferrite is 50% or more.
[0047] Next, the reasons for limiting the chemical components in the present invention are
explained.
[0048] C is an indispensable element for obtaining a desired microstructure. When a C content
exceeds 0.3%, however, workability deteriorates and, for this reason, a C content
is limited to 0.3% or less. Additionally, when a C content exceeds 0.2%, weldability
tends to deteriorate and, for this reason, it is desirable that a C content is 0.2%
or less. On the other hand, when a C content is less than 0.01%, steel strength decreases
and, therefore, a C content is limited to 0.01% or more. Further, for the purpose
of obtaining retained austenite stably in an amount sufficient for realizing a good
ductility, it is desirable that a C content is 0.05% or more.
[0049] Si is a solute-strengthening element and, as such, it is effective for enhancing
strength. An Si content has to be 0.01% or more for obtaining a desired strength,
but, when an Si content exceeds 2%, workability deteriorates. Therefore, an Si content
is limited in the range from 0.01 to 2%.
[0050] Mn is also a solute-strengthening element and, as such, it is effective for enhancing
strength. An Mn content has to be 0.05% or more for obtaining a desired strength.
In the case where elements such as Ti, which suppress hot cracking induced by S, are
not added in a sufficient amount in addition to Mn, it is desirable to add Mn so that
the expression Mn/S ≧ 20 is satisfied in terms of mass percentage. Further, Mn is
an element that stabilizes austenite and, therefore, in order to stably obtain a sufficient
amount of retained austenite in an attempt to secure a good ductility, it is desirable
that an Mn addition amount is 0.1% or more. When Mn is added in excess of 3%, on the
other hand, cracks occur to a slab. For this reason, an Mn content is limited to 3%
or less.
[0051] P is an undesirable impurity, and the lower the P content, the better. When a P content
exceeds 0.1%, workability and weldability are adversely affected, and so are fatigue
properties. Therefore, a P content is limited to 0.1% or less.
[0052] S is also an undesirable impurity, and the lower the S content, the better. When
an S content is too high, the A type inclusions detrimental to local ductility and
burring workability are formed and, for this reason, an S content has to be minimized.
A permissible content of S is 0.01% or less.
[0053] Al must be added by 0.005% or more for deoxidizing molten steel, but its upper limit
is set at 1.0% to avoid a cost increase. Al increases the formation of non-metallic
inclusions and deteriorates elongation when added excessively and, for this reason,
a desirable content of Al is 0.5% or less.
[0054] Cu is added as occasion demands, since Cu has an effect of improving fatigue properties
when it is in the state of solid solution. No tangible effect is obtained when a Cu
addition amount is less than 0.2%, but the effect is saturated when a Cu content exceeds
2%. Thus, the range of a Cu content is determined to be from 0.2 to 2%. It has to
be noted that, when a coiling temperature is 450°C or higher and Cu is added in excess
of 1.2%, Cu may precipitate after coiling, drastically deteriorating workability.
For this reason, it is desirable to limit a Cu content to 1.2% or less.
[0055] B is added as occasion demands, as B has an effect of raising fatigue limit when
added in combination with Cu. An addition of B by less than 0.0002% is not enough
for obtaining the effect, but, when B is added in excess of 0.002%, cracks occur in
a slab. For this reason, the addition amount of B is limited to 0.0002 to 0.002%.
[0056] Ni is added as occasion demands for preventing hot shortness caused by the presence
of Cu. An Ni addition amount of less than 0.1% is not enough for obtaining the effect,
but, even when it is added in excess of 1%, the effect is saturated. For this reason,
an Ni content is limited in the range from 0.1 to 1%.
[0057] Ca and REM are the elements that modify the shape of non-metallic inclusions, which
serve as the starting points of fractures and/or deteriorate workability, and, by
so doing, render them harmless. But no tangible effect is obtained when either of
them is added at less than 0.0005%. When Ca is added in excess of 0.002% or REM in
excess of 0.02%, the effect is saturated. Thus, it is desirable to add Ca by 0.0005
to 0.002% and REM by 0.0005 to 0.02%.
[0058] Additionally, one or more of precipitation-strengthening and solute-strengthening
elements, namely Ti, Nb, Mo, V, Cr and Zr, may be added for enhancing strength. However,
when they are added at less than 0.05%, 0.01%, 0.05%, 0.02%, 0.01% and 0.02%, respectively,
no tangible effects are obtained and, when they are added in excess of 0.5, 0.5%,
1%, 0.2%, 1% and 0.2%, respectively, their effects are saturated.
[0059] Note that Sn, Co, Zn, W and/or Mg may be added at 1% or less in total to a steel
containing aforementioned elements as the main components. However, as Sn may cause
surface defects during hot rolling, it is desirable to limit an Sn content to 0.05%
or less.
[0060] Now, the reasons for limiting the conditions of the production method according to
the present invention are explained in detail hereafter.
[0061] A steel sheet according to the present invention can be produced through any of the
following process routes: casting, hot rolling and cooling; casting, hot rolling,
cooling, pickling, cold rolling and annealing; heat treatment of a hot-rolled or cold-rolled
steel sheet in a hot dip plating line; or, further, surface treatment applied separately
to a steel sheet produced through any of the above process routes.
[0062] The present invention does not specify production methods prior to hot rolling. That
is, a steel may be melted and refined in a blast furnace, an electric arc furnace
or the like, then the chemical components may be adjusted in one or more of various
secondary refining processes so that the steel may contain desired amounts of the
components, and then the steel may be cast into a slab through a casting process such
as an ordinary continuous casting process, an ingot casting process and a thin slab
casting process. Steel scraps may be used as a raw material. Further, in the case
of a slab cast through a continuous casting process, the slab may be fed to a hot-rolling
mill directly while it is hot, or it may be hot rolled after being cooled to room
temperature and then heated in a reheating furnace.
[0063] No limit is particularly set to the temperatures of reheating, but it is desirable
that a reheating temperature is lower than 1,400°C, since, when it is 1,400°C or higher,
the descale amount becomes large and the product yield decreases. It is also desirable
that a reheating temperature is 1,000°C or higher, since a reheating temperature lower
than 1,000°C remarkably deteriorates the operation efficiency of a rolling mill in
terms of rolling schedule.
[0064] In a hot rolling process, a slab undergoes finish rolling after completing rough
rolling. When descaling is applied after completing the rough rolling, it is desirable
to satisfy the following condition:

where, P (MPa) is an impact pressure of high-pressure water on a steel sheet surface,
andL (l/cm
2) a flow rate of descaling water.
[0065] An impact pressure P of high-pressure water on a steel sheet surface is expressed
as follows (see Tetsu-to-Hagané, 1991, Vol. 77, No. 9, p.1450):

where, P
0 (MPa) is a pressure of liquid, V (l/min.) a liquid flow rate of a nozzle, and H (cm)
a distance between a nozzle and the surface of a steel sheet.
[0066] The flow rate L (l/cm
2) is expressed as follows:

where, V (l/min.) is a liquid flow rate of a nozzle, W (cm) the width of liquid when
the liquid blown from a nozzle hits a steel sheet surface, and v (cm/min.) a traveling
speed of a steel sheet.
[0067] It is not necessary to specify an upper limit of the product of the impact pressure
P and the flow rate L for the purpose of obtaining the effects of the present invention.
However, it is preferable that the product is 0.02 or less because, when the liquid
flow rate of a nozzle is raised, problems such as violent nozzle wear occur.
[0068] It is preferable, further, that the maximum roughness height Ry of a steel sheet
after finish rolling is 15 µm (15 µm Ry, ℓ 2.5 mm, ℓn 12.5 mm) or less. The reason
for this is clear from the fact that the fatigue strength of an as-hot-rolled or as-pickled
steel sheet correlates with the maximum roughness height Ry of the steel sheet surface,
as stated, for example, in page 84 of Metal Material Fatigue Design Handbook edited
by the Society of Materials Science, Japan. Further, it is preferable that the subsequent
finish hot rolling is done within 5 sec. after high-pressure descaling so that scales
may be prevented from forming again.
[0069] Besides the above, finish rolling may be carried out continuously by welding sheet
bars together after rough rolling or the subsequent descaling. In this case, the rough-rolled
sheet bars may be welded together after being coiled temporarily, held inside a cover
having a heat retention function as occasion demands, and then uncoiled.
[0070] When a hot-rolled steel sheet is used as a final product, it is necessary that the
finish rolling is done at a total reduction ratio of 25% or more in the temperature
range of the Ar
3 transformation temperature + 100°C or lower during the latter half of the finish
rolling. Here, the Ar
3 transformation temperature can be expressed, in a simplified manner, in relation
to steel chemical components, for instance, by the following equation:

[0071] When the total reduction ratio in the temperature range of the Ar
3 transformation temperature + 100°C or lower is less than 25%, the rolled texture
of austenite does not develop sufficiently and, as a result, the effects of the present
invention are not obtained, no matter how the steel sheet is cooled thereafter. For
obtaining the specified texture, it is desirable that the total reduction ratio in
the temperature range of the Ar
3 transformation temperature + 100°C or lower is 35% or more.
[0072] The present invention does not specify a lower limit of the temperature range in
which rolling at a total reduction ratio of 25% or more is carried out. However, when
the rolling is done at a temperature lower than the Ar
3 transformation temperature, a work-induced structure remains in ferrite having precipitated
during the rolling, and, as a result, ductility falls and workability deteriorates.
For this reason, it is desirable that a lower limit of the temperature range in which
rolling at a total reduction ratio of 25% or more is carried out is not lower than
the Ar
3 transformation temperature. However, when recovery or recrystallization advances
to some extent during the subsequent coiling process or a heat treatment after the
coiling process, a rolling temperature lower than the Ar
3 transformation temperature is acceptable.
[0073] The present invention does not specify an upper limit of the total reduction ratio
in the temperature range of the Ar
3 transformation temperature + 100°C or lower. However, when a total reduction ratio
exceeds 97.5%, the rolling load becomes too high and it becomes necessary to increase
the rigidity of a rolling mill excessively, resulting in economical disadvantage.
For this reason, the total reduction ratio is, desirably, 97.5% or less.
[0074] Here, when the friction between a hot-rolling roll and a steel sheet is large during
hot rolling in the temperature range of the Ar
3 transformation temperature + 100°C or lower, crystal orientations mainly composed
of {110} planes develop at planes near the surfaces of the steel sheet, causing the
deterioration of notch-fatigue strength. As a countermeasure, lubrication may be applied
for reducing the friction between a hot-rolling roll and a steel sheet as occasion
demands.
[0075] The present invention does not specify an upper limit of the friction coefficient
between a hot-rolling roll and a steel sheet. However, when a friction coefficient
exceeds 0.2, crystal orientations mainly composed of {110} planes develop conspicuously,
deteriorating notch-fatigue strength. For this reason, it is desirable to control
a friction coefficient between a hot-rolling roll and a steel sheet to 0.2 or less
at least at one of the passes of the hot rolling in the temperature range of the Ar
3 transformation temperature + 100°C or lower. It is more desirable to control a friction
coefficient between a hot-rolling roll and a steel sheet to 0.15 or less at all the
passes of the hot rolling in the temperature range of the Ar
3 transformation temperature + 100°C or lower.
[0076] Here, a friction coefficient between a hot-rolling roll and a steel sheet is the
value calculated from a forward slip ratio, a rolling load, a rolling torque and so
on on the basis of the rolling theory.
[0077] The present invention does not specify a temperature at the final pass (FT) of finish
rolling, but it is desirable that the final pass is completed at a temperature not
lower than the Ar
3 transformation temperature. This is because, if a rolling temperature is lower than
the Ar
3 transformation temperature during hot rolling, a work-induced structure remains in
ferrite having precipitated before or during the rolling, and, as a result, ductility
lowers and workability deteriorates. However, when a heat treatment for recovery or
recrystallization is applied during or after the subsequent coiling process, a temperature
at the final pass (FT) of finish rolling is allowed to be lower than the Ar
3 transformation temperature.
[0078] The present invention does not specify an upper limit of a finishing temperature,
but, if a finishing temperature exceeds the Ar
3 transformation temperature + 100°C, it becomes practically impossible to carry out
rolling at a total reduction ratio of 25% or more in the temperature range of the
Ar
3 transformation temperature + 100°C or lower. For this reason, it is desirable that
an upper limit of a finishing temperature is the Ar
3 transformation temperature + 100°C or lower.
[0079] In the present invention, it is not necessary to specify the microstructure of a
steel sheet for only the purpose of enhancing the notch-fatigue strength thereof and,
therefore, no specific limitation is set forth regarding the cooling process after
the completion of finish rolling until the coiling at a prescribed coiling temperature.
Nevertheless, a steel sheet is cooled, as occasion demands, for the purpose of securing
a prescribed coiling temperature or controlling the microstructure. The present invention
does not specify an upper limit of a cooling rate, but, as thermal strain may cause
a steel sheet to warp, it is desirable to control a cooling rate to 300°C/sec. or
lower. In addition, when a cooling rate is too high, it becomes impossible to accurately
control the cooling end temperature and an over-cooling may happen as a result of
overshooting to a temperature lower than a prescribed coiling temperature. For this
reason, a cooling rate here is, desirably, 150°C/sec. or lower. No lower limit of
a cooling rate is specifically set forth, either. For reference, the cooling rate
in the case where a steel sheet is left to cool by air without any intentional cooling
is 5°C/sec. or higher.
[0080] For the purpose of obtaining a good burring workability in addition to enhancing
notch-fatigue strength in the present invention, it is necessary that the microstructure
of a steel sheet is a compound structure containing bainite or ferrite and bainite
as the phase accounting for the largest volume percentage. In that case, the present
invention does not specify the conditions of the process after the completion of finish
rolling until the coiling at a prescribed coiling temperature, except for the cooling
rate applied during the process. However, in the case where a steel sheet is required
to have both a good burring workability and a high ductility without sacrificing the
burring workability too much, a hot-rolled steel sheet may be retained for 1 to 20
sec. in the temperature range from the Ar
3 transformation temperature to the Ar
1 transformation temperature (the ferrite-austenite two-phase zone). Here, the retention
of a hot-rolled steel sheet is carried out for accelerating ferrite transformation
in the two-phase zone. When a retention time is less than 1 sec., ferrite transformation
in the two-phase zone is insufficient and a sufficient ductility is not obtained.
However, when a retention time exceeds 20 sec., pearlite forms and an intended microstructure
having a compound structure containing bainite or ferrite and bainite as the phase
accounting for the largest volume percentage is not obtained.
[0081] In addition, in order to facilitate the acceleration of ferrite transformation, it
is desirable that the temperature range in which a steel sheet is retained for 1 to
20 sec. is from the Ar
1 transformation temperature to 800°C. Further, in order not to lower productivity
drastically, it is desirable that the retention time, which has been defined earlier
as in the range from 1 to 20 sec., is 1 to 10 sec. For satisfying all those requirements,
it is necessary to reach said temperature range rapidly at a cooling rate of 20°C/sec.
or higher after completing finish rolling.
[0082] The present invention does not specify an upper limit of a cooling rate, but, in
consideration of the capacity of cooling equipment, a reasonable cooling rate is 300°C/sec.
or lower. In addition, when a cooling rate is too high, it becomes impossible to accurately
control the cooling end temperature and over-cooling may occur as a result of overshooting
to the Ar
1 transformation temperature or lower, losing the ductility improvement effect. For
this reason, a cooling rate here is, desirably, 150°C/sec. or lower.
[0083] Subsequently, a steel sheet is cooled at a cooling rate of 20°C/sec. or higher from
the above temperature range to a coiling temperature (CT). When a cooling rate is
lower than 20°C/sec., pearlite or bainite containing carbides forms and an intended
microstructure having a compound structure containing bainite or ferrite and bainite
as the phase accounting for the largest volume percentage is not obtained. The effects
of the present invention can be enjoyed without specifying an upper limit of the cooling
rate down to the coiling temperature but, to avoid warping caused by thermal strain,
it is desirable to control a cooling rate to 300°C/sec. or lower.
[0084] For the purpose of obtaining a good ductility in addition to enhancing notch-fatigue
strength in the present invention, it is necessary that the microstructure of a steel
sheet is a compound structure containing retained austenite at 5 to 25% in terms of
volume percentage and having the balance mainly consisting of ferrite and bainite.
For obtaining such a compound structure, a hot-rolled steel sheet has to be retained
for 1 to 20 sec. in the temperature range from the Ar
3 transformation temperature to the Ar
1 transformation temperature (the ferrite-austenite two-phase zone) in the first process
after completing finish rolling. Here, the retention of a hot-rolled steel sheet is
carried out for accelerating ferrite transformation in the two-phase zone. When a
retention time is less than 1 sec., ferrite transformation in the two-phase zone is
insufficient and a sufficient ductility is not obtained. However, when a retention
time exceeds 20 sec., pearlite forms and an intended microstructure containing retained
austenite by 5 to 25% in terms of volume percentage and having the balance mainly
consisting of ferrite and bainite is not obtained.
[0085] In addition, in order to facilitate the acceleration of ferrite transformation, it
is desirable that the temperature range in which a steel sheet is retained for 1 to
20 sec. is from the Ar
1 transformation temperature to 800°C. Further, in order not to lower productivity
drastically, it is desirable that the retention time, which has been defined earlier
as in the range from 1 to 20 sec., is 1 to 10 sec. To satisfy all those requirements,
it is necessary to reach said temperature range rapidly at a cooling rate of 20°C/sec.
or higher after completing finish rolling. The present invention does not specify
an upper limit of a cooling rate, but, in consideration of the capacity of cooling
equipment, a reasonable cooling rate is 300°C/sec. or lower. In addition, when a cooling
rate is too high, it becomes impossible to accurately control the cooling end temperature
and over-cooling may happen as a result of overshooting to the Ar
1 transformation temperature or lower. For this reason, a cooling rate here is, desirably,
150°C/sec. or lower.
[0086] Subsequently, a steel sheet is cooled at a cooling rate of 20°C/sec. or higher from
the above temperature range to a coiling temperature (CT). When a cooling rate is
lower than 20°C/sec., pearlite or bainite containing carbides forms and a sufficient
amount of retained austenite is not secured and, as a result, an intended microstructure
containing retained austenite at 5 to 25% in terms of volume percentage and having
the balance mainly consisting of ferrite and bainite is not obtained. The effects
of the present invention can be enjoyed without bothering to specify an upper limit
of the cooling rate down to the coiling temperature but, to avoid warping caused by
thermal strain, it is desirable to control a cooling rate to 300°C/sec. or lower.
[0087] Further, for the purpose of obtaining a low yield ratio for realizing a good shape-fixation
property in addition to enhancing notch-fatigue strength in the present invention,
it is necessary that the microstructure of a steel sheet is a compound structure containing
ferrite as the phase accounting for the largest volume percentage and mainly martensite
as the second phase. For obtaining such a compound structure, a hot-rolled steel sheet
has to be retained for 1 to 20 sec. in the temperature range from the Ar
3 transformation temperature to the Ar
1 transformation temperature (the ferrite-austenite two-phase zone) in the first process
after completing finish rolling. Here, the retention of a hot-rolled steel sheet is
carried out for accelerating ferrite transformation in the two-phase zone. When a
retention time is less than 1 sec., ferrite transformation in the two-phase zone is
insufficient and a sufficient ductility is not obtained. However, when a retention
time exceeds 20 sec., pearlite forms and an intended compound structure containing
ferrite as the phase accounting for the largest volume percentage and mainly martensite
as the second phase is not obtained.
[0088] In addition, in order to facilitate the acceleration of ferrite transformation, it
is desirable that the temperature range in which a steel sheet is retained for 1 to
20 sec. is from the Ar
1 transformation temperature to 800°C. Further, in order not to lower productivity
drastically, it is desirable that the retention time, which has been defined earlier
as in the range from 1 to 20 sec., is 1 to 10 sec. To satisfy all those requirements,
it is necessary to reach said temperature range rapidly at a cooling rate of 20°C/sec.
or higher after completing finish rolling. The present invention does not specify
an upper limit of a cooling rate, but, in consideration of the capacity of cooling
equipment, a reasonable cooling rate is 300°C/sec. or lower. In addition, when a cooling
rate is too high, it becomes impossible to accurately control the cooling end temperature
and over-cooling may happen as a result of overshooting to the Ar
1 transformation temperature or lower. For this reason, a cooling rate here is, desirably,
150°C/sec. or lower.
[0089] Subsequently, a steel sheet is cooled at a cooling rate of 20°C/sec. or higher from
the above temperature range to a coiling temperature (CT). When a cooling rate is
lower than 20°C/sec., pearlite or bainite forms and a sufficient amount of martensite
is not secured and, as a result, an intended microstructure containing ferrite as
the phase accounting for the largest volume percentage and martensite as the second
phase is not obtained.
[0090] The effects of the present invention can be enjoyed without specifying an upper limit
of the cooling rate down to the coiling temperature but, to avoid distortion caused
by thermal strain, it is desirable to control the cooling rate to 300°C/sec. or lower.
[0091] In the present invention, it is not necessary to specify the microstructure of a
steel sheet only for the purpose of enhancing the notch-fatigue strength thereof and,
therefore, the present invention does not specify an upper limit of a coiling temperature.
However, in order to carry over the texture of austenite obtained by finish rolling
at a total reduction ratio of 25% or more in the temperature range of the Ar
3 transformation temperature + 100°C or lower, it is desirable to coil a steel sheet
at the coiling temperature T
0 shown below or lower. Note that it is unnecessary to set the temperature T
0 to room temperature or lower. T
0 is the temperature defined thermodynamically as that at which austenite and ferrite
having the same chemical components as the austenite have the same free energy. It
can be calculated in a simplified manner by the following equation, taking the influences
of components other than C into consideration:

where, B is determined as follows:

where, Mneq is determined from the mass percentages of the component elements as
shown below:

[0092] Note that the influences on T
0 of the mass percentages of the other components specified in the present invention
than those included in the above equation are insignificant, and are negligible here.
[0093] Since it is not necessary to specify the microstructure of a steel sheet only for
the purpose of enhancing the notch-fatigue strength thereof, it is not necessary to
specify the lower limit of a coiling temperature. However, to avoid a poor appearance
caused by rust when a coil is kept wet with water for a long period of time, it is
desirable that a coiling temperature is not lower than 50°C.
[0094] For the purpose of obtaining a good burring workability in addition to enhancing
notch-fatigue strength in the present invention, it is necessary that the microstructure
of a steel sheet is a compound structure containing bainite or ferrite and bainite
as the phase accounting for the largest volume percentage. To obtain such a compound
structure, the coiling temperature has to be restricted to 450°C or higher. This is
because, when a coiling temperature is lower than 450°C, retained austenite or martensite
considered detrimental to burring workability may form in a great amount and, as a
consequence, an intended microstructure having a compound structure containing bainite
or ferrite and bainite as the phase accounting for the largest volume percentage is
not obtained.
[0095] Further, although the present invention does not specify a cooling rate to be applied
after coiling, it is desirable that a cooling rate after coiling is 30°C/sec. or higher
to a temperature of 200°C. Otherwise, when Cu is added by 1.2% or more, it precipitates
after coiling and, as a result, not only workability is deteriorated but also solute
Cu effective for improving fatigue properties may be lost.
[0096] Further, for the purpose of obtaining a good ductility in addition to enhancing notch-fatigue
strength in the present invention, it is necessary that the microstructure of a steel
sheet is a compound structure containing retained austenite at 5 to 25% in terms of
volume percentage and having the balance mainly consisting of ferrite and bainite.
To obtain such a compound structure, the coiling temperature is restricted to lower
than 450°C. This is because, when a coiling temperature is 450°C or higher, bainite
containing carbides forms and a sufficient amount of retained austenite is not secured
and, as a result, an intended microstructure containing retained austenite at 5 to
25% in terms of volume percentage, and having the balance mainly consisting of ferrite
and bainite, is not obtained. When a coiling temperature is not higher than 350°C,
on the other hand, a great amount of martensite forms and a sufficient amount of retained
austenite is not secured and, as a result, an intended microstructure containing retained
austenite by 5 to 25% in terms of volume percentage and having the balance mainly
consisting of ferrite and bainite is not obtained. For this reason, a coiling temperature
is limited to higher than 350°C.
[0097] Further, although the present invention does not specify a cooling rate to be applied
after coiling, it is desirable that a cooling rate after coiling is 30°C/sec. or higher
up to a temperature of 200°C. Otherwise, when Cu is added at 1% or more, it precipitates
after coiling and, as a result, not only is the workability deteriorated but also
solute Cu effective for improving fatigue properties may be lost.
[0098] Further, for the purpose of obtaining a low yield ratio for realizing a good shape-fixation
property in addition to enhancing notch-fatigue strength in the present invention,
it is necessary that the microstructure of a steel sheet is a compound structure containing
ferrite as the phase accounting for the largest volume percentage and mainly martensite
as the second phase. For obtaining such a compound structure, a coiling temperature
has to be restricted to 350°C or lower. This is because, when a coiling temperature
exceeds 350°C, bainite forms and a sufficient amount of martensite is not secured
and, as a result, an intended microstructure containing ferrite as the phase accounting
for the largest volume percentage and martensite as the second phase is not obtained.
It is not necessary to specify a lower limit of a coiling temperature but, to avoid
a poor appearance caused by rust when a coil is kept wet with water for a long period
of time, it is desirable that a coiling temperature is not lower than 50°C.
[0099] After completing a hot rolling process, as occasion demands, a steel sheet may be
subjected to pickling and then skin pass rolling at a reduction ratio of 10% or less
or cold rolling at a reduction ratio up to 40% or so, either on-line or off-line.
[0100] Next, in the case where a cold-rolled steel sheet is used as a final product, the
present invention does not specify the conditions of finish hot rolling. However,
in order to obtain a better notch-fatigue strength, it is desirable that a total reduction
ratio, in the temperature range of the Ar
3 transformation temperature + 100°C or lower, is 25% or more. Further, while the temperature
at the final pass (FT) of finish rolling is allowed to be lower than the Ar
3 transformation temperature, in such a case, since an intensively work-induced structure
remains in ferrite having precipitated before or during the rolling, it is desirable
that the work-induced structure is recovered and recrystallized through the subsequent
coiling process or a heat treatment.
[0101] A total reduction ratio at subsequent cold rolling after pickling must be less than
80%. This is because, when a total reduction ratio at cold rolling is 80% or more,
the ratios of the integrated X-ray diffraction strengths in {111} and {554} crystallographic
planes parallel to the plane of a steel sheet, the crystallographic planes having
a texture usually obtained through cold rolling and recrystallization, tend to rise.
A preferable total reduction ratio at cold rolling is 70% or less. The effects of
the present invention can be enjoyed without specifying a lower limit of a cold reduction
ratio but, for controlling the X-ray diffraction strengths in specific crystal orientation
components within appropriate ranges, it is desirable to set a lower limit of a cold
reduction ratio at 3% or more.
[0102] The discussion here is based on the premise that the heat treatment of a steel sheet
cold rolled as specified above is carried out in a continuous annealing process.
[0103] In the first place, a steel sheet is subjected to a heat treatment for 5 to 150 sec.
in the temperature range of the Ac
3 transformation temperature + 100°C or lower. When an upper limit of a heat treatment
temperature exceeds the Ac
3 transformation temperature + 100°C, ferrite having formed through recrystallization
transforms into austenite, the texture formed by the growth of austenite grains is
randomized, and the texture of ferrite finally obtained is also randomized. For this
reason, an upper limit of a heat treatment temperature is set at the Ac
3 transformation temperature + 100°C or lower.
[0104] The Ac
1 and Ac
3 transformation temperatures mentioned herein can be expressed in relation to steel
chemical components using, for example, the expressions according to p. 273 of the
Japanese translation of The Physical Metallurgy of Steels by W. C. Leslie (published
by Maruzen in 1985, translated by Hiroshi Kumai and Tatsuhiko Noda).
[0105] With regard to a lower limit of a heat treatment temperature, it is acceptable if
the temperature is equal to or higher than the recovery temperature, because it is
not necessary to specify the microstructure of a steel sheet for the purpose of enhancing
the notch-fatigue strength thereof. When a heat treatment temperature is lower than
the recovery temperature, however, a work-induced structure is retained and formability
is significantly deteriorated. For this reason, a lower limit of a heat treatment
temperature is set to be equal to or higher than the recovery temperature. Further,
with regard to a retention time in the above temperature range, when a retention time
is shorter than 5 sec., it is insufficient for having cementite completely dissolve
again. However, when a retention time exceeds 150 sec., the effect of the heat treatment
is saturated and, what is worse, productivity is lowered. For this reason, a retention
time is determined to be in the range from 5 to 150 sec.
[0106] The present invention does not specify the conditions of cooling after a heat treatment.
However, for the purpose of controlling the microstructure of a steel sheet, cooling
or the combination of retention at an arbitrary temperature and cooling as explained
later may be employed as deemed necessary.
[0107] For the purpose of obtaining a good burring workability in addition to enhancing
notch-fatigue strength in the present invention, it is necessary that the microstructure
of a steel sheet is a compound structure containing bainite or ferrite and bainite
as the phase accounting for the largest volume percentage. To obtain such a compound
structure, a lower limit of a heat treatment temperature is set at a temperature of
the Ac
1 transformation temperature or higher. When a lower limit of a heat treatment temperature
is lower than the Ac
1 transformation temperature, an intended compound structure containing bainite or
ferrite and bainite as the phase accounting for the largest volume percentage, is
not obtained. When it is intended to obtain both a good burring workability and a
high ductility without sacrificing the burring workability too much, a heat treatment
temperature must be in the range from the Ac
1 transformation temperature to the Ac
3 transformation temperature (the ferrite-austenite two-phase zone) in order to increase
the volume percentage of ferrite. Further, for the purpose of obtaining a still better
burring workability, it is desirable that the heat treatment temperature is in the
range from the Ac
3 transformation temperature to the Ac
3 transformation temperature + 100°C in order to increase the volume percentage of
bainite.
[0108] The present invention does not specify the conditions of a cooling process in heat
treatment. However, when a heat treatment temperature is in the range from the Ac
1 transformation temperature to the Ac
3 transformation temperature, it is desirable to cool a steel sheet at a cooling rate
of 20°C/sec. or higher to the temperature range from higher than 350°C to the temperature
T
0 specified herein earlier. This is because, when a cooling rate is lower than 20°C/sec.,
the temperature history of steel is likely to pass through the transformation nose
of bainite or pearlite containing much carbide. Further, when a cooling end temperature
is 350°C or lower, martensite, which is considered detrimental to burring properties,
may form in a great amount and, as a result, an intended microstructure having a compound
structure containing bainite or ferrite and bainite as the phase accounting for the
largest volume percentage is not obtained. For this reason, it is desirable that a
cooling end temperature is higher than 350°C. In addition, in order to carry over
the texture obtained to the previous process, it is desirable that a cooling end temperature
is not higher than T
0.
[0109] Finally, when a cooling rate to the cooling end temperature is 20°C/sec. or higher,
martensite, which is considered detrimental to burring properties, may form in a great
amount during the cooling and, as a result, an intended microstructure having a compound
structure containing bainite or ferrite and bainite as the phase accounting for the
largest volume percentage may not be obtained. For this reason, it is desirable that
a cooling rate is lower than 20°C/sec. Further, when a cooling end temperature is
higher than 200°C, aging properties may deteriorate, and, for this reason, it is desirable
that a cooling end temperature is 200°C or lower. If water cooling or mist cooling
is applied and a coil is kept wet with water for a long period of time, it is desirable,
to avoid a poor appearance caused by rust, that a cooling end temperature is not lower
than 50°C.
[0110] On the other hand, in the case where above mentioned heat treatment temperature is
in the range from higher than the Ac
3 transformation temperature to the Ac
3 transformation temperature + 100°C, it is desirable to cool a steel sheet at a cooling
rate of 20°C/sec. or higher to a temperature of 200°C or lower. This is because, when
a cooling rate is lower than 20°C/sec., the temperature history of steel is likely
to pass through the transformation nose of bainite or pearlite containing much carbide.
In addition, when a cooling end temperature exceeds 200°C, aging properties may deteriorate.
For this reason, it is desirable that a cooling end temperature is 200°C or lower.
If water cooling or mist cooling is applied and a coil is kept wet with water for
a long period of time, it is desirable, to avoid a poor appearance caused by rust,
that a cooling end temperature is not lower than 50°C.
[0111] Further, for the purpose of obtaining a good ductility in addition to enhancing notch-fatigue
strength in the present invention, it is necessary that the microstructure of a steel
sheet is a compound structure containing retained austenite at 5 to 25% in terms of
volume percentage and having the balance mainly consisting of ferrite and bainite.
To obtain such a compound structure, a steel sheet must be subjected to a heat treatment
for 5 to 150 sec. in the temperature range from the Ac
1 transformation temperature to the Ac
3 transformation temperature + 100°C, as described earlier. In this case, when a temperature
is too low within the above temperature range and when cementite has precipitated
in an as-hot-rolled state, it takes too long for the cementite to dissolve again.
When a temperature is too high, on the other hand, the volume percentage of austenite
increases excessively and the concentration of C in austenite decreases, and, as a
consequence, the temperature history of steel is likely to pass through the transformation
nose of bainite or pearlite containing much carbide. For this reason, it is desirable
to heat a steel sheet to a temperature in the range from 780°C to 850°C. When a cooling
rate after retention is lower than 20°C/sec., the temperature history of steel is
likely to pass through the transformation nose of bainite or pearlite containing much
carbide, and, for this reason, a cooling rate must be 20°C/sec. or higher.
[0112] Next, with respect to the process to accelerate bainite transformation and stabilize
a required amount of retained austenite, when a cooling end temperature is not lower
than 450°C, retained austenite is decomposed into bainite or pearlite containing much
carbide, and an intended microstructure containing retained austenite at 5 to 25%
in terms of volume percentage and having the balance mainly consisting of ferrite
and bainite is not obtained. When a cooling end temperature is not higher than 350°C,
on the other hand, martensite may form in a great amount and a sufficient amount of
retained austenite cannot be secured and, as a result, an intended microstructure
containing retained austenite at 5 to 25% in terms of volume percentage and the balance
mainly consisting of ferrite and bainite is not obtained. For this reason, the cooling
must be continued to a temperature in the range from higher than 350°C to lower than
450°C.
[0113] Further, with respect to a retention time in the above temperature range, when a
retention time is shorter than 5 sec., bainite transformation for stabilizing retained
austenite is insufficient and, as a consequence, unstable retained austenite may transform
into martensite at the end of the subsequent cooling, and, as a result, an intended
microstructure containing retained austenite at 5 to 25% in terms of volume percentage
and having the balance mainly consisting of ferrite and bainite is not obtained. When
a retention time exceeds 600 sec., on the other hand, bainite transformation overshoots
and a required amount of stable retained austenite is not formed, and, as a result,
an intended microstructure containing retained austenite at 5 to 25% in terms of volume
percentage and having the balance mainly consisting of ferrite and bainite is not
obtained. For this reason, a retention time in the above temperature range must be
from 5 to 600 sec.
[0114] Finally, when a cooling rate up to the end of cooling is lower than 5°C/sec., bainite
transformation may overshoot during the cooling and a required amount of stable retained
austenite is not formed, and, as a consequence, an intended microstructure containing
retained austenite by 5 to 25% in terms of volume percentage and having the balance
mainly consisting of ferrite and bainite may not be obtained. For this reason, a cooling
rate is set at 5°C/sec. or higher.
[0115] In addition, when a cooling end temperature is higher than 200°C, aging properties
may deteriorate and, for this reason, a cooling end temperature must be 200°C or lower.
The present invention does not specify a lower limit for a cooling end temperature.
However, if water cooling or mist cooling is applied and a coil is kept wet with water
for a long period of time, it is desirable, to avoid a poor appearance caused by rust,
that a cooling end temperature is not lower than 50°C.
[0116] Further, for the purpose of obtaining a low yield ratio for realizing a good shape-fixation
property in addition to enhancing notch-fatigue strength in the present invention,
it is necessary that the microstructure of a steel sheet is a compound structure containing
ferrite as the phase accounting for the largest volume percentage and mainly martensite
as the second phase. To obtain such a compound structure, a steel sheet must be subjected
to a heat treatment for 5 to 150 sec. in the temperature range from the Ac
1 transformation temperature to the Ac
3 transformation temperature + 100°C as described before. In this case, when the temperature
is too low within the above temperature range and when cementite has precipitated
in an as-hot-rolled state, it takes too long for the cementite to dissolve again.
When the temperature is too high, on the other hand, the volume percentage of austenite
increases excessively and the concentration of C in austenite decreases, and, as a
consequence, the temperature history of steel is likely to pass through the transformation
nose of bainite or pearlite containing much carbide. For this reason, it is desirable
to heat a steel sheet to a temperature in the range from 780°C to 850°C.
[0117] When a cooling rate after retention is lower than 20°C/sec., the temperature history
of steel is likely to pass through the transformation nose of bainite or pearlite
containing much carbide, and, for this reason, a cooling rate must be 20°C/sec. or
higher. When a cooling end temperature is higher than 350°C, an intended microstructure
containing ferrite as the phase accounting for the largest volume percentage and martensite
as the second phase is not obtained. For this reason, the cooling must be continued
down to a temperature of 350°C or lower. The present invention does not specify a
lower limit of a cooling end temperature. However, if water cooling or mist cooling
is applied and a coil is kept wet with water for a long period of time, it is desirable,
to avoid a poor appearance caused by rust, that a cooling end temperature is not lower
than 50°C.
[0118] Thereafter, skin pass rolling may be applied, if required.
[0119] When galvanizing is applied to a hot-rolled steel sheet after pickling or a cold-rolled
steel sheet after completing the above annealing for recrystallization, the steel
sheet is dipped in a zinc-plating bath. After that, it may be subjected to an alloying
treatment, if required.
Example
(Example 1)
[0120] The present invention is further explained hereafter based on Example 1.
[0121] Steels A to L having the chemical components shown in Table 1 were melted and refined
in a converter, cast continuously into slabs, reheated and then rolled through rough
rolling and finish rolling into steel sheets 1.2 to 5.5 mm in thickness, and then
coiled. Note that the chemical components in the table are expressed in terms of mass
percentage.
[0122] Table 2 shows the details of the production conditions. In the table, "SRT" means
the slab reheating temperature, "FT" the finish rolling temperature at the final pass,
and "reduction ratio" the total reduction ratio in the temperature range of the Ar
3 transformation temperature + 100°C or lower. Note that, in the case where a hot-rolled
steel sheet is cold rolled, it is not necessary to restrict the reduction ratio of
hot rolling and, for this reason, the space of "reduction ratio" is filled with a
dash meaning "not applicable." Further, "lubrication" indicates if or not lubrication
is applied in the temperature range of the Ar
3 transformation temperature + 100°C or lower.
[0123] In the column of "coiling", ○ means that the coiling temperature (CT) is equal to
or lower than T
0, and × that the coiling temperature is higher than T
0. Note that, in the case of a cold-rolled steel sheet, the space is filled with a
dash meaning "not applicable," because it is not necessary to restrict the coiling
temperature as one of the production conditions.
[0124] Some of the steel sheets were subjected to pickling, cold rolling and annealing after
hot rolling. The thickness of the cold-rolled steel sheets ranged from 0.7 to 2.3
mm.
[0125] Also in the table, "cold reduction ratio" means the total reduction ratio of the
cold rolling, and "time" the time of annealing. In the column of "annealing", ○ means
that the annealing temperature is within the range from the recovery temperature to
the Ar
3 transformation temperature + 100°C, and × that it is outside the range. Steel L was
subjected to descaling under the conditions of an impact pressure of 2.7 MPa and a
flow rate of 0.001 l/cm
2 after the rough rolling. Further, among the steels mentioned above, steels G and
F-5 were subjected to zinc plating.
[0126] The hot-rolled steel sheets thus prepared were subjected to a tensile test in accordance
with the test method specified in JIS Z 2241, after forming the specimens into No.
5 test pieces according to JIS Z 2201. The yield strength (σY), tensile strength (σB)
and breaking elongation (El) of the steel sheets are shown also in Table 2.
[0127] Then, a test piece 30 mm in diameter was cut out from a position of 1/4 or 3/4 of
the width of each of the steel sheets, the surfaces were ground to a depth of about
0.05 mm so that the surfaces might have the three-triangle grade finish (the second
finest finish) and, subsequently, strain was removed by chemical polishing or electrolytic
polishing. The test pieces thus prepared were subjected to X-ray diffraction strength
measurement in accordance with the method described in pages 274 to 296 of the Japanese
translation of Elements of X-ray Diffraction by B. D. Cullity (published in 1986 by
AGNE Gijutsu Center, translated by Gentaro Matsumura).
[0128] Here, the average of the ratios of the X-ray diffraction strength in the orientation
component group of {100}<011> to {223}<110> to random X-ray diffraction strength is
obtained from the X-ray diffraction strengths in the principal orientation components
included in the orientation component group, namely {100}<011>, {116}<110>, {114}<110>,
{113}<110>, {112}<110>, {335}<110> and {223}<110>, in the three-dimensional texture
calculated either by the vector method based on the pole figure of {110} or by the
series expansion method using two or more (desirably, three or more) pole figures
out of the pole figures of {110}, {100}, {211} and {310}.
[0129] For example, in the case of obtaining the ratios of the X-ray diffraction strength
in the above crystal orientation components to random X-ray diffraction strength by
the latter method, the strengths of (001)[1-10], (116)[1-10], (114)[1-10], (113)[1-10],
(112)[1-10], (335)[1-10] and (223)[1-10] at a φ2 = 45° cross section in a three-dimensional
texture may be used without modification. Note that the average of the ratios of the
X-ray diffraction strength in the orientation component group of {100}<011> to {223}<110>
to random X-ray diffraction strength is the arithmetic average of the ratios in all
the above orientation components.
[0130] When it is impossible to obtain the strengths in all these orientation components,
the arithmetic average of the strengths in the orientation components of {100}<011>,
{116}<110>, {114}<110>, {112}<110> and {223}<110> may be used as a substitute.
[0131] Likewise, the average of the ratios of the X-ray diffraction strength in the three
orientation components of {554}<225>, {111}<112> and {111}<110> to random X-ray diffraction
strength can be obtained from the three-dimensional texture calculated in the same
manner as explained above.
[0132] In Table 2, "strength ratio 1" under "ratios of X-ray diffraction strength to random
X-ray diffraction strength" means the average of the ratios of the X-ray diffraction
strength in the orientation component group of {100}<011> to {223}<110> to random
X-ray diffraction strength, and "strength ratio 2" the average of the ratios of the
X-ray diffraction strength in the above three orientation components of {554}<225>,
{111}<112> and {111}<110> to random X-ray diffraction strength.
[0133] Next, for the purpose of investigating the notch-fatigue strength of the above steel
sheets, a test piece for fatigue test having the shape shown in Fig. 1(b) was cut
out from a position of 1/4 or 3/4 of the width of each of the steel sheets so that
the longitudinal direction of the test piece coincided with the rolling direction
of the steel sheet, and subjected to a fatigue test. The surfaces of the test pieces
for fatigue test were ground to a depth of about 0.05 mm so that the surfaces might
have the second finest finish, and the fatigue test was carried out using an electro-hydraulic
servo type fatigue tester and methods conforming to JIS Z 2273-1978 and Z 2275-1978.
The notch-fatigue limit (σWK) and notch-fatigue limit ratio (σWK/σB) of each of the
steel sheets are shown also in Table 2.
[0134] The samples according to the present invention are 11 steels, namely steels A, E,
F-1, F-2, F-5, G, H, I, J, K and L. In these samples, obtained are the thin steel
sheets for automobile use excellent in notch-fatigue strength, each of the steel sheets
being characterized in that: the steel sheet contains prescribed amounts of chemical
components; on a plane at an arbitrary depth within 0.5 mm from the surface of the
steel sheet in the thickness direction thereof, the average of the ratios of the X-ray
diffraction strength in the orientation component group of {100}<011> to {223}<110>
to random X-ray diffraction strength is 2 or more and the average of the ratios of
the X-ray diffraction strength in the three orientation components of {554}<225>,
{111}<112> and {111}<110> to random X-ray diffraction strength is 4 or less; and the
thickness of the steel sheet is in the range from 0.5 to 12 mm. As a consequence,
in the evaluations by the methods according to the present invention, the fatigue
limit ratios of these steels were superior to those of conventional steels which ranged
from 20 to 30%.
[0135] All the steels other, than those mentioned above, in the tables were outside the
ranges of the present invention for the following reasons.
[0136] In steel B, the content of C was outside the range specified in the present invention
and, as a consequence, a sufficient strength (σB) was not obtained. In steel C, the
content of P was outside the range specified in the present invention and, as a consequence,
a sufficient notch-fatigue strength ratio (σWK/σB) was not obtained. In steel D, the
content of S was outside the range specified in the present invention and, as a consequence,
a sufficient elongation (El) was not obtained. In steel F-3, as the total reduction
ratio in the temperature range of the Ar
3 transformation temperature + 100°C or lower was outside the range specified in the
present invention, the texture intended in the present invention was not obtained
and, as a consequence, a sufficient notch-fatigue strength ratio (σWK/σB) was not
obtained.
[0137] In steel F-4, as the finish rolling end temperature (FT) and the coiling temperature
were outside the respective ranges specified in the present invention, the texture
intended in the present invention was not obtained and, as a consequence, a sufficient
notch-fatigue strength ratio (σWK/σB) was not obtained. In steel F-6, as the cold
reduction ratio was outside the range specified in the present invention, the texture
intended in the present invention was not obtained and, as a consequence, a sufficient
notch-fatigue strength ratio (σWK/σB) was not obtained. In steel F-7, as the annealing
temperature was outside the range specified in the present invention, the texture
intended in the present invention was not obtained and, as a consequence, a sufficient
notch-fatigue strength ratio (σWK/σB) was not obtained. In steel F-8, as the annealing
time was outside the range specified in the present invention, the texture intended
in the present invention was not obtained and, as a consequence, a sufficient notch-fatigue
strength ratio (σWK/σB) was not obtained.
(Example 2)
[0138] The present invention is hereafter explained in more detail based on Example 2.
[0139] Slabs of two steels G and H having the chemical components shown in Table 1 were
reheated to the reheating temperatures shown in Table 3, rolled through rough rolling
and then finish rolling into steel sheets 1.5 to 5.5 mm in thickness, and then coiled.
As shown in Table 3, some of the steel sheets were subjected to descaling under the
conditions of an impact pressure of 2.7 MPa and a flow rate of 0.001 l/cm
2 after the rough rolling.
[0140] Table 3 shows the details of the production conditions. In the table, "SRT" means
the slab reheating temperature, "FT" the finish rolling temperature at the final pass,
and "reduction ratio" the total reduction ratio in the temperature range of the Ar
3 transformation temperature + 100°C or lower. Note that, in the case where a hot-rolled
steel sheet is cold rolled, it is not necessary to restrict the reduction ratio of
hot rolling and, for this reason, the space "reduction ratio" is filled with a dash
meaning "not applicable." Further, "lubrication" indicates if or not lubrication is
applied in the temperature range of the Ar
3 transformation temperature + 100°C or lower. Furthermore, "CT" indicates the coiling
temperature. Note that, in the case of a cold-rolled steel sheet, the space is filled
with a dash meaning "not applicable," because it is not necessary to restrict the
coiling temperature as one of the production conditions. Some of the steel sheets
were subjected to pickling, cold rolling and heat treatment after the hot rolling.
The thickness of the cold-rolled steel sheets ranged from 0.7 to 2.3 mm. Also in the
table, "cold reduction ratio" means the total reduction ratio of the cold rolling,
"ST" the temperature of the heat treatment and "time" the time thereof. Some of the
steels were subjected to galvanizing .
[0141] The hot-rolled and cold-rolled steel sheets thus prepared were subjected to a tensile
test in the same manner as described earlier.
[0142] The yield strength (σY), tensile strength (σB), breaking elongation (El), yield ratio
(YR) and strength-ductility index (σB x El) of each of the steel sheets are shown
in Table 4. Burring workability (hole expansibility) was evaluated following the hole
expansion test method according to the Standard of the Japan Iron and Steel Federation
JFS T 1001-1996. Table 4 also shows the hole expansion ratio (λ).
[0143] Table 4 shows the microstructures of the steel sheets, too. Here, "others" accounts
for pearlite and any other phase than ferrite, bainite, retained austenite and martensite,
which are listed individually in Table 4. The volume percentage of ferrite, bainite,
retained austenite, pearlite or martensite is defined as the area percentage thereof
in the microstructure of each of the steel sheets observed with an optical microscope
under a magnification of 200 to 500 at a position in the depth of 1/4 of the steel
sheet thickness on a section surface along the rolling direction of a specimen which
is cut out from a position of 1/4 or 3/4 of the width of the steel sheet, the section
surface being polished and etched with a nitral reagent and the reagent disclosed
in Japanese Unexamined Patent Publication No. H5-163590.
[0144] Because the crystal structure of austenite is different from that of ferrite, they
can be easily distinguished from each other crystallographically. Therefore, the volume
percentage of retained austenite can be obtained experimentally by the X-ray diffraction
method too, namely by the simplified method wherein the volume percentage thereof
is calculated with the following equation on the basis of the difference between austenite
and ferrite in the reflection intensity of the Kα ray of Mo on their lattice planes:

where, α(211), γ(220) and γ(311) are the X-ray reflection intensities of the indicated
lattice planes of ferrite (α) and austenite (γ), respectively. The measurement result
of the volume percentage of retained austenite was substantially the same either by
the optical microscope observation or the X-ray diffraction method, and, thus, the
measured values by any of the two methods may be used.
[0145] The X-ray diffraction strength was measured by the same method as described earlier.
[0146] The fatigue test was carried out also in the same manner as described earlier. The
notch-fatigue limit (σWK) and notch-fatigue limit ratio (σWK/σB) of the steel sheets
are shown also in Table 4.
[0147] The samples according to the present invention are 9 steels, namely steels g-1, g-2,
g-3, g-5, g-6, g-7, h-1, h-2 and h-3. In these samples, obtained are thin steel sheets,
for automobile use, excellent in notch-fatigue strength, each of the steel sheets
being characterized in that: the steel sheet contains prescribed amounts of chemical
components; on a plane at an arbitrary depth within 0.5 mm from the surface of the
steel sheet in the thickness direction thereof, the average of the ratios of the x-ray
diffraction strength in the orientation component group of {100}<011> to {223}<110>
to random X-ray diffraction strength is 2 or more and the average of the ratios of
the X-ray diffraction strength in the three orientation components of {554}<225>,
{111}<112> and {111}<110> to random X-ray diffraction strength is 4 or less; the thickness
of the steel sheet is in the range from 0.5 to 12 mm; and the microstructure is a
compound structure containing bainite or ferrite and bainite as the phase accounting
for the largest volume percentage, a compound structure containing retained austenite
by 5 to 25% in terms of volume percentage and having the balance mainly consisting
of ferrite and bainite, or a compound structure containing ferrite as the phase accounting
for the largest volume percentage and mainly martensite as the second phase. As a
consequence, in the evaluations by the methods according to the present invention,
the fatigue limit ratios of these steels were significantly superior to those of conventional
steels which ranged from 20 to 30%.
[0148] All the steels, other than those mentioned above, in the table were outside the ranges
of the present invention for the following reasons.
[0149] In steel g-4, as the finish rolling end temperature (FT) and the total reduction
ratio in the temperature range of the Ar
3 transformation temperature + 100°C or lower were outside the respective ranges specified
in the present invention, the texture intended in the present invention was not obtained
and, as a consequence, a sufficient notch-fatigue strength ratio (σWK/σB) was not
obtained. In steel g-8, as the cold reduction ratio was outside the range specified
in the present invention, the texture intended in the present invention was not obtained
and, as a consequence, a sufficient notch-fatigue strength ratio (σWK/σB) was not
obtained. In steel h-4, too, as the finish rolling end temperature (FT) and the total
reduction ratio in the temperature range of the Ar
3 transformation temperature + 100°C or lower were outside the respective ranges specified
in the present invention, the texture intended in the present invention was not obtained
and, as a consequence, a sufficient notch-fatigue strength ratio (σWK/σB) was not
obtained.

Effect of the Invention
[0150] As has been explained in detail, the present invention relates to a thin steel sheet,
for automobile use, excellent in notch-fatigue strength, and a method for producing
the steel sheet. The use of a thin steel sheet according to the present invention
makes it possible to expect a significant improvement in notch-fatigue strength that
is one of the essential properties of such a structural member including an undercarriage
component of an automobile to overcome the problem of generating the propagation of
a fatigue crack from a site of stress concentration including a blanked or welded
portion and thus to require durability. For this reason, the present invention is
of a high industrial value.
1. A thin steel sheet, for automobile use, excellent in notch-fatigue strength, characterized in: that, on a plane at an arbitrary depth within 0.5 mm from the surface of the steel sheet
in the thickness direction thereof, the average of the ratios of the X-ray diffraction
strength in the orientation component group of {100}<011> to {223}<110> to random
X-ray diffraction strength is 2 or more and the average of the ratios of the X-ray
diffraction strength in the three orientation components of {554}<225>, {111}<112>
and {111}<110> to random X-ray diffraction strength is 4 or less; and that the thickness
of the steel sheet is in the range from 0.5 to 12 mm.
2. A thin steel sheet, for automobile use, excellent in notch-fatigue strength according
to claim 1, characterized in that the microstructure of the steel sheet is a compound structure containing bainite
or ferrite and bainite as the phase accounting for the largest volume percentage.
3. A thin steel sheet, for automobile use, excellent in notch-fatigue strength according
to claim 1, characterized in that the microstructure of the steel sheet is a compound structure containing retained
austenite at 5 to 25% in terms of volume percentage and having the balance mainly
consisting of ferrite and bainite.
4. A thin steel sheet for automobile use excellent in notch-fatigue strength according
to claim 1, characterized in that the microstructure of the steel sheet is a compound structure containing ferrite
as the phase accounting for the largest volume percentage and martensite as the second
phase.
5. A thin steel sheet for automobile use excellent in notch-fatigue strength, the steel
sheet containing, in mass, 0.01 to 0.3% C, 0.01 to 2% Si, 0.05 to 3% Mn, 0.1% or less
P, 0.01% or less S and 0.005 to 1% Al, with the balance consisting of Fe and unavoidable
impurities, characterized in that, on a plane at an arbitrary depth within 0.5 mm from the surface of the steel sheet
in the thickness direction thereof, the average of the ratios of the X-ray diffraction
strength in the orientation component group of {100}<011> to {223}<110> to random
X-ray diffraction strength is 2 or more and the average of the ratios of the X-ray
diffraction strength in the three orientation components of {554}<225>, {111}<112>
and {111}<110> to random X-ray diffraction strength is 4 or less and that the thickness
of the steel sheet is in the range from 0.5 to 12 mm.
6. A thin steel sheet for automobile use excellent in notch-fatigue strength according
to claim 5, characterized by further containing, in mass, one or more of 0.2 to 2% Cu, 0.0002 to 0.002% B, 0.1
to 1% Ni, 0.0005 to 0.002% Ca, 0.0005 to 0.02% REM, 0.05 to 0.5% Ti, 0.01 to 0.5%
Nb, 0.05 to 1% Mo, 0.02 to 0.2% V, 0.01 to 1% Cr and 0.02 to 0.2% Zr.
7. A thin steel sheet for automobile use excellent in notch-fatigue strength according
to claim 5 or 6, characterized in that the microstructure of the steel sheet is any one of 1) a compound structure containing
bainite or ferrite and bainite as the phase accounting for the largest volume percentage,
2) a compound structure containing retained austenite at 5 to 25% in terms of volume
percentage and having the balance mainly consisting of ferrite and bainite, and 3)
a compound structure containing ferrite as the phase accounting for the largest volume
percentage and martensite as the second phase.
8. A thin steel sheet for automobile use excellent in notch-fatigue strength, characterized in that the steel sheet is produced by applying galvanizing to a thin steel sheet for automobile
use according to any one of claims 1 to 7.
9. A method for producing a thin steel sheet for automobile use excellent in notch-fatigue
strength characterized in that a steel slab containing, in mass, 0.01 to 0.3% C, 0.01 to 2% Si, 0.05 to 3% Mn, 0.1%
or less P, 0.01% or less S and 0.005 to 1% Al, with the balance consisting of Fe and
unavoidable impurities, is subjected, in a hot rolling process, to rough rolling and
then to finish rolling at a total reduction ratio of 25% or more in terms of steel
sheet thickness in the temperature range of the Ar3 transformation temperature + 100°C or lower, that, on a plane at an arbitrary depth
within 0.5 mm from the surface of the steel sheet in the thickness direction thereof,
the average of the ratios of the X-ray diffraction strength in the orientation component
group of {100}<011> to {223}<110> to random X-ray diffraction strength is 2 or more
and the average of the ratios of the X-ray diffraction strength in the three orientation
components of {554}<225>, {111}<112> and {111}<110> to random X-ray diffraction strength
is 4 or less and that the thickness of the steel sheet is in the range from 0.5 to
12 mm.
10. A method for producing a thin steel sheet, for automobile use, excellent in notch-fatigue
strength according to claim 9, characterized by cooling the steel sheet at a cooling rate of 20°C/sec. or higher after the finish
rolling and then coiling it at a coiling temperature of 450°C or higher.
11. A method for producing a thin steel sheet, for automobile use, excellent in notch-fatigue
strength according to claim 9, characterized by retaining the steel sheet for 1 to 20 sec. in the temperature range from the Ar1 transformation temperature to the Ar3 transformation temperature after the finish rolling then cooling it at a cooling
rate of 20°C/sec. or higher and then coiling it at a coiling temperature in the range
from higher than 350°C to lower than 450°C.
12. A method for producing a thin steel sheet, for automobile use, excellent in notch-fatigue
strength according to claim 11, characterized by coiling the steel sheet at a coiling temperature of 350°C or lower after the cooling.
13. A method for producing a thin steel sheet, for automobile use, excellent in notch-fatigue
strength according to any one of claims 9 to 12, characterized by applying lubrication rolling to the steel sheet in the hot rolling.
14. A method for producing a thin steel sheet, for automobile use, excellent in notch-fatigue
strength according to any one of claims 9 to 13, characterized by applying descaling to the steel sheet after the completion of the rough rolling in
the hot rolling.
15. A method for producing a thin steel sheet, for automobile use, excellent in notch-fatigue
strength, characterized in that a steel slab containing, in mass, 0.01 to 0.3% C, 0.01 to 2% Si, 0.05 to 3% Mn, 0.1%
or less P, 0.01% or less S and 0.005 to 1% Al, with the balance consisting of Fe and
unavoidable impurities, is subjected to rough rolling, then finish rolling at a total
reduction ratio of 25% or more in terms of steel sheet thickness in the temperature
range of the Ar3 transformation temperature + 100°C or lower, pickling, cold rolling at a reduction
ratio of less than 80% in terms of steel sheet thickness and then annealing for recovery
or recrystallization comprising the processes of retaining the cold-rolled steel sheet
for 5 to 150 sec. in the temperature range from the recovering temperature to the
Ac3 transformation temperature + 100°C and then cooling it, that, on a plane at an arbitrary
depth within 0.5 mm from the surface of the steel sheet in the thickness direction
thereof, the average of the ratios of the X-ray diffraction strength in the orientation
component group of {100}<011> to {223}<110> to random X-ray diffraction strength is
2 or more and the average of the ratios of the X-ray diffraction strength in the three
orientation components of {554}<225>, {111}<112> and {111}<110> to random X-ray diffraction
strength is 4 or less and that the thickness of the steel sheet is in the range from
0.5 to 12 mm.
16. A method for producing a thin steel sheet, for automobile use, excellent in notch-fatigue
strength according to claim 15, characterized by subjecting the steel sheet after the cold rolling to a heat treatment comprising
the processes of retaining the cold-rolled steel sheet for 5 to 150 sec. in the temperature
range from the AC1 transformation temperature to the Ac3 transformation temperature + 100°C and then cooling it.
17. A method for producing a thin steel sheet for automobile use excellent in notch-fatigue
strength according to claim 15, characterized by subjecting the steel sheet to a heat treatment comprising the processes of, in sequence,
retaining the cold-rolled steel sheet for 5 to 150 sec. in said temperature range,
cooling it at a cooling rate of 20°C/sec. or higher to the temperature range from
higher than 350°C to lower than 450°C, retaining it for 5 to 600 sec. in said temperature
range, and then cooling it at a cooling rate of 5°C/sec. or higher to the temperature
range of 200°C or lower.
18. A method for producing a thin steel sheet, for automobile use, excellent in notch-fatigue
strength according to claim 15, characterized in subjecting the steel sheet to a heat treatment comprising the processes of retaining
the cold-rolled steel sheet for 5 to 150 sec. in said temperature range and then cooling
it at a cooling rate of 20°C/sec. or higher to the temperature range of 350°C or lower.
19. A method for producing a thin steel sheet, for automobile use, excellent in notch-fatigue
strength, characterized in that the steel sheet produced by the method according to any one of claims 11 to 18 further
contains, in mass, one or more of 0.2 to 2% Cu, 0.0002 to 0.002% B, 0.1 to 1% Ni,
0.0005 to 0.002% Ca, 0.0005 to 0.02% REM, 0.05 to 0.5% Ti, 0.01 to 0.5% Nb, 0.05 to
1% Mo, 0.02 to 0.2% V, 0.01 to 1% Cr and 0.02 to 0.2% Zr.
20. A method for producing a thin steel sheet, for automobile use, excellent in notch-fatigue
strength according to claim 10 or 16, characterized in that the microstructure of the steel sheet is a compound structure containing bainite
or ferrite and bainite as the phase accounting for the largest volume percentage.
21. A method for producing a thin steel sheet, for automobile use, excellent in notch-fatigue
strength according to claim 11 or 17, characterized in that the microstructure of the steel sheet is a compound structure containing retained
austenite at 5 to 25% in terms of volume percentage and having the balance mainly
consisting of ferrite and bainite.
22. A method for producing a thin steel sheet, for automobile use, excellent in notch-fatigue
strength according to claim 12 or 18, characterized in that the microstructure of the steel sheet is a compound structure containing ferrite
as the phase accounting for the largest volume percentage and martensite as the second
phase.
23. A method for producing a thin steel sheet, for automobile use, excellent in notch-fatigue
strength characterized by, after producing a hot-rolled steel sheet or a steel sheet annealed for recovery
or recrystallization according to any one of claims 9 to 22, further applying galvanizing
to the surfaces of the steel sheet by dipping the steel sheet in a zinc plating bath.
24. A method for producing a thin steel sheet, for automobile use, excellent in notch-fatigue
strength according to claim 23, characterized by further subjecting the steel sheet to an alloying treatment after the galvanizing.