Technical Field
[0001] The present invention relates to steel sheet and a method of production of the same.
Background Art
[0002] Steel sheet containing, by mass%, carbon in an amount of 0.1 to 0.7% is being used
as a material for production of gears, clutches, and other drive system parts of automobiles
by being used press-formed, enlarged in holes, bent, drawn, thickened, and thinned
and cold forged by combinations of the same from a blank. The strength of such parts
is secured by quenching and tempering, so a high hardenability is demanded from steel
sheet.
[0003] Furthermore, a high formability in the cold state is demanded from steel sheet used
as a material for such drive system parts. Parts are mainly formed by drawing and/or
thickening. In forming parts, the biggest factor governing the material formability
is the plastic anisotropy. Improvement of the plastic anisotropy in steel sheet is
necessary for application of steel sheet to the formation of parts.
[0004] Several proposals have been made up to now for the hardenability demanded and formability
improved in plastic anisotropy. The following patent literature discloses steel sheet
excellent in cold forgeability and impact resistance characteristic.
[0005] For example, PLT 1 discloses, as steel for machine structural use improving toughness
by suppressing coarsening of crystal grains in carburization heat treatment, steel
for machine structural use containing, by mass%, C: 0.10 to 0.30%, Si: 0.05 to 2.0%,
Mn: 0.10 to 0.50%, P: 0.030% or less, S: 0.030% or less, Cr: 1.80 to 3.00%, Al: 0.005
to 0.050%, Nb: 0.02 to 0.10%, and N: 0.0300% or less and having a balance of Fe and
unavoidable impurities, having a structure before cold working comprised of ferrite
and pearlite structures, and having an average value of ferrite grain size of 15 µm
or more.
[0006] PLT 2 discloses, as steel excellent in cold workability and carburizing and quenching
ability, steel containing C: 0.15 to 0.40%, Si: 1.00% or less, Mn: 0.40% or less,
sol. Al: 0.02% or less, N: 0.006% or less, and B: 0.005 to 0.050%, having a balance
of Fe and unavoidable impurities, and having a structure mainly comprised of ferrite
phases and graphite phases.
[0007] PLT 3 discloses a steel material for carburized bevel gear use excellent in impact
strength, a high toughness carburized bevel gear, and a method of production of the
same.
[0008] PLT 4 discloses, for a part produced by spheroidal annealing, then a cold forging
and a carburizing, quenching, and tempering process, steel for carburized part use
having excellent workability while suppressing coarsening of crystal grains even with
subsequent carburization and having an excellent impact resistance characteristic
and impact fatigue resistance characteristic.
[0009] PLT 5 discloses as cold tool steel for plasma carburization use a steel containing
C: 0.40 to 0.80%, Si: 0.05 to 1.50%, Mn: 0.05 to 1.50%, and V: 1.8 to 6.0%, further
containing one or more of Ni: 0.10 to 2.50%, Cr: 0.1 to 2.0%, and Mo: 3.0% or less,
and having a balance of Fe and unavoidable impurities.
[0010] On the other hand, there have been the following proposals for improvement of the
formability, that is, the improvement of plastic anisotropy.
[0011] For example, PLT 6 proposes prescribing the carbide grain size and spheroidization
rate in steel containing C: 0.25 to 0.75% and improving the in-plane anisotropy by
the cold rolling rate and box annealing conditions, the coiling temperature in hot
rolling, and provisions on the texture so as to limit the "r" value and Δr.
[0012] PLTs 7 and 8 propose to prescribe the heating and annealing conditions of a hot rolled
material between stands of a finish rolling machine so as to reduce the Δr value and
improve the in-plane anisotropy. PLT 8 proposes steel sheet reduced in in-plane anisotropy
by prescribing hot rolling during which performing finish rolling at a temperature
of the Ar3 point or more and coiling at 500 to 630°C.
Citation List
Patent Literature
Summary of Invention
Technical Problem
[0014] The above patent literature proposed improvement of the in-plane anisotropy, but
did not propose the provision of the strength demanded from the part, that is, the
hardenability.
[0015] The present invention was made in consideration of the above situation in the prior
art and has as its object the provision of steel sheet improved in hardenability and
material formability, in particular, optimal for obtaining a gear or other part by
thickening or other cold forging, and a method of production of the same.
Solution to Problem
[0016] To solve the above problem and obtain steel sheet suitable for the material of a
drive system part etc., it can be understood that in steel sheet containing the C
necessary for raising the hardenability, it is sufficient to increase the grain size
of the ferrite, spheroidize the carbides (mainly cementite) by a suitable grain size,
and decrease the pearlite structures. This is due to the following reasons.
[0017] Ferrite phases are low in hardness and high in ductility. Therefore, in a structure
mainly comprised of ferrite, it becomes possible to increase the grain size so as
to raise the material formability.
[0018] Carbides, by being made to suitably disperse in the metal structure, can maintain
the material formability while imparting an excellent wear resistance and rolling
fatigue characteristic, so are structures essential for drive system parts. Further,
the carbides in the steel sheet are strong particles obstructing slip. By forming
carbides at the ferrite grain boundaries, it is possible to prevent propagation of
slip exceeding the crystal grain boundaries and suppress the formation of shear zones.
The cold forgeability is improved and, simultaneously, the formability of steel sheet
is also improved.
[0019] However, cementite is a hard, brittle structure. If a laminar structure with ferrite
present, that is, in the state of pearlite, the steel becomes hard and brittle, so
it has to be present in a spheroidal form. If considering the cold forgeability and
the occurrence of fractures at the time of forging, its grain size has to be a suitable
range.
[0020] However, no method of production for realizing the above structure has been disclosed
up to now. Therefore, the inventors intensively researched a method of production
for realizing the above structure.
[0021] As a result, they discovered the following: To make the metal structure of the steel
sheet after coiling after hot rolling a bainite structure of fine pearlite or fine
ferrite with small lamellar spacing in which cementite is dispersed, the steel sheet
is coiled at a relatively low temperature (400°C to 550°C). By coiling at a relatively
low temperature, the cementite dispersed in the ferrite also easily becomes spheroidal.
Next, the cementite is partially made spheroidal by annealing at a temperature just
under the Ac1 point as first stage annealing. Next, as second stage annealing, part
of the ferrite grains is left while part is transformed to austenite by annealing
at a temperature between the Ac1 point and Ac3 point (so-called dual phase region
of ferrite and austenite). By then making the remaining ferrite grains grow while
slowly cooling the steel while using these as nuclei to transform the austenite to
ferrite, it is possible to obtain large ferrite phases and make cementite precipitate
at the grain boundaries to realize the above structure.
[0022] That is, the inventors found that it is difficult to realize a method of production
of steel sheet satisfying both hardenability and formability even if adjusting the
heat rolling conditions, annealing conditions, etc. separately and that it is possible
to realize this by optimization by a so-called integrated process of hot rolling,
annealing, etc.
[0023] Further, they found that for improvement of the drawability at the time of cold forming,
reduction of the plastic anisotropy is necessary and, to improve this, adjustment
of the hot rolling conditions is important.
[0024] The present invention was made based on these findings and has as its gist the following:
- (1) A steel sheet consisting of, by mass%, C: 0.10 to 0.70%, Si: 0.01 to 0.30%, Mn:
0.30 to 3.00%, Al: 0.001 to 0.10%, Cr: 0.010 to 0.50%, Mo: 0.0010 to 0.50%, B: 0.0004
to 0.01%, Ti: 0.001 to 0.10%, P: 0.02% or less, S: 0.01% or less, N: 0.0200% or less,
O: 0.0200% or less, Sn: 0.05% or less, Sb: 0.05% or less, As: 0.05% or less, Nb: 0.10%
or less, V: 0.10% or less, Cu: 0.10% or less, W: 0.10% or less, Ta: 0.10% or less,
Ni: 0.10% or less, Mg: 0.05% or less, Ca: 0.05% or less, Y: 0.05% or less, Zr: 0.05%
or less, La: 0.05% or less, and Ce: 0.05% or less and a balance of Fe and unavoidable
impurities, wherein the metal structure of the steel sheet includes carbide having
an average grain size of 0.4 µm to 2.0 µm, perlite having an area ratio of 6% or less,
and ferrite wherein a ratio of a number of carbides at ferrite grain boundaries to
a number of carbides in ferrite grains of over 1; and I1/I0<1 being satisfied when
an X-ray diffraction intensity at {211}<011> at a plane of a part of 1/2 sheet thickness
of the steel sheet is denoted by "I1" and an X-ray diffraction intensity at {100}<011>
is denoted by "10", the steel sheet having a Vickers hardness of 100 HV to 150 HV.
- (2) A method of production for producing steel sheet according to (1) comprising hot
rolling a steel slab of a chemical composition according to (1) with finish rolling
temperature between 820°C and 950°C, to obtain hot rolled steel sheet; coiling the
hot rolled steel sheet at 400°C to 550°C; pickling the coiled hot rolled steel sheet;
heating the pickled hot rolled steel sheet to an annealing temperature of 650°C to
720°C by a heating rate of 30°C/hour to 150°C/hour and holding the steel sheet for
3 hours to 60 hours as a first stage of annealing; next, heating the hot rolled steel
sheet to an annealing temperature of 725°C to 790°C by a heating rate of 1°C/hour
to 80°C/hour and holding the steel sheet for 3 hours to less than 10 hours as a second
stage of annealing; and, next, cooling the annealed hot rolled steel sheet to 650°C
by a cooling rate of 1°C/hour to 100°C/hour.
Advantageous Effects of Invention
[0025] According to the present invention, it is possible to provide steel sheet excellent
in hardenability and material formability, in particular, optimal for obtaining a
gear or other part by forming by thickening or other cold forging, and a method of
production of the same.
Description of Embodiments
[0026] Below, the present invention will be explained in detail. First, the reasons for
limitation of the chemical composition of the steel sheet of the present invention
will be explained. Here, the "%" according to the chemical composition means "mass%".
C: 0.10 to 0.70%
[0027] C is an element forming carbides and effective for strengthening the steel and refining
the ferrite grains. To suppress the formation of a matte surface in cold working and
secure surface beauty of a cold forged part, suppression of coarsening of the ferrite
grain size is necessary.
[0028] If C is less than 0.10%, the carbides become insufficient in volume fraction and
coarsening of the carbides during annealing can no longer be suppressed, so C is made
0.10% or more. Preferably it is 0.14% or more. On the other hand, if the content of
C increases, the carbides increase in volume fraction, cracks are formed acting as
starting points of breakage at the time of an instantaneous load, and there is the
fear that the formability and impact resistance characteristic will fall. If making
this drop as small as possible, C is made 0.40% or less. Preferably it is 0.38% or
less.
[0029] On the other hand, if the carbides increase in volume fraction and the strength rises,
the fatigue characteristic is improved, so when improving the fatigue characteristic,
C is made over 0.40%. Preferably it is 0.44% or more. If C is over 0.70%, a large
amount of cracks forming starting points of breakage are formed and the fatigue characteristic
conversely falls, so C is made 0.70% or less. Preferably it is 0.66% or less.
Si: 0.01 to 0.30%
[0030] Si is an element which acts as a deoxidizing agent and further has an effect on the
form of the carbides and contributes to the improvement of the material formability.
To obtain the deoxidizing effect, Si is made 0.01% or more. Preferably it is 0.07%
or more.
[0031] If Si is over 0.30%, due to solution strengthening of the ferrite, the hardness rises
and the ductility falls, fractures easily occur at the time of cold forging, and the
formability at the time of cold forging and the impact resistance characteristic after
carburization, quenching, and temperature falls, so Si is made 0.30% or less. Preferably
it is 0.28% or less.
Mn: 0.30 to 3.00%
[0032] Mn is an element controlling the form of carbides in two-stage annealing. If less
than 0.30%, in the gradual cooling after second stage annealing, it becomes difficult
to form carbides at the ferrite grain boundaries, so Mn is made 0.30% or more. Preferably
it is 0.40% or more.
[0033] If Mn is over 1.00%, after carburization, quenching, and tempering, the toughness
falls, but on the other hand, the strength rises. When trying to keep down the drop
in toughness after carburization, quenching, and tempering as much as possible Mn
is made 1.00% or less. Preferably it is 0.96% or less.
[0034] When trying to raise the strength, Mn is made over 1.00%. Preferably it is 1.10%
or more. If Mn is over 3.00%, after carburization, quenching, and tempering, the toughness
remarkably falls, so Mn is made 3.00% or less. Preferably it is 2.70% or less.
Al: 0.001 to 0.10%
[0035] Al is an element which acts as a deoxidizing agent and stabilizes ferrite. If less
than 0.001%, the effect of addition is not sufficiently obtained, so Al is made 0.001%
or more. Preferably it is 0.004% or more.
[0036] On the other hand, if Al is over 0.10%, the number of carbides at the ferrite grain
boundaries decreases and the formability falls, so Al is made 0.10% or less. Preferably
it is 0.09% or less.
Cr: 0.010 to 0.50%
[0037] Cr is an element effective for stabilization of carbides at the time of heat treatment.
If less than 0.010%, it becomes difficult to cause carbides to remain at the time
of carburization, coarsening of the austenite grain size at the surface layer is invited,
and the strength drops, so Cr is made 0.010% or more. Preferably it is 0.050% or more.
[0038] On the other hand, if Cr is over 0.50%, the amount of Cr concentrating at the carbides
increases and a large amount of fine carbides remain in the austenite phases produced
by the two-stage annealing, carbides remain in the ferrite grains after gradual cooling
inviting an increase in the hardness and a decrease in the number of carbides at the
ferrite grain boundaries fall, and the formability falls, so Cr is made 0.50% or less.
Preferably it is 0.40% or less.
Mo: 0.001 to 0.50%
[0039] Mo, like Mn and Cr, is an element effective for control of the form of carbides.
If less than 0.001%, the effect of addition is not obtained, so Mo is made 0.001%
or more. Preferably it is 0.005% or more.
[0040] On the other hand, if over 0.50%, Mo concentrates at the carbides, stable carbides
increase even in the austenite phases, carbides remain inside the ferrite grains after
gradual cooling inviting an increase in the hardness and a decrease in the number
of carbides at the ferrite grain boundaries, and the material formability falls, so
Mo is made 0.50% or less. Preferably it is 0.40% or less.
B: 0.0004 to 0.01%
[0041] B is an element raising the hardenability and further raising the toughness. In the
steel sheet of the present invention, a predetermined hardenability is required, so
0.0004 to 0.01% is added. If less than 0.0004%, the effect of addition is not obtained,
so B is made 0.0004% or more. Preferably it is 0.0010% or more.
[0042] On the other hand, if over 0.01%, coarse B compounds becoming the cause of internal
defects and other flaws at the time of steel production are formed, so B is made 0.01%
or less. Preferably it is 0.007% or less.
Ti: 0.001 to 0.10%
[0043] Ti is an element forming nitrides and contributing to refinement of the crystal grains
and works to effectively bring out the effect of addition of B. If less than 0.001%,
the effect of addition is not obtained, so Ti is made 0.001% or more. Preferably it
is 0.010% or more.
[0044] On the other hand, if over 0.10%, coarse Ti nitrides are formed and the material
formability falls, so Ti is made 0.10% or less. Preferably it is 0.07% or less.
[0045] The following elements are impurities and have to be controlled to certain amounts
or less.
P: 0.02% or less
[0046] P is an element segregating at the ferrite grain boundaries and working to suppress
the formation of carbides at the ferrite grain boundaries. For this reason, the smaller
the amount of P, the better. The content of P may also be 0, but if reducing it to
less than 0.0001%, the refining costs greatly increase, so the substantive lower limit
is 0.0001 to 0.0013%.
[0047] If P is over 0.02%, formation of carbides at the ferrite grain boundaries is suppressed,
the number of carbides decreases, and the material formability falls, so P is made
0.02% or less. Preferably it is 0.01% or less.
S: 0.01% or less
[0048] S is an impurity element forming MnS and other nonmetallic inclusions. The nonmetallic
inclusions form starting points of fracture at the time of cold forging, so the smaller
the S, the better. The content of S may also be 0, but to lower S to less than 0.0001%,
the refining costs greatly increase, so the substantive lower limit is 0.0001 to 0.0012%.
[0049] If S is over 0.01%, nonmetallic inclusions are formed and the material formability
falls, so S is made 0.01% or less. Preferably it is 0.009% or less.
N: 0.02% or less
[0050] N is an element which, if present in a large amount, causes embrittlement of the
ferrite. For this reason, the smaller the amount of N, the better. The content of
N may also be 0, but to lower N to less than 0.0001%, the refining costs greatly increase,
so the substantive lower limit is 0.0001 to 0.0006%.
[0051] If N is over 0.02%, the ferrite becomes brittle and the material formability falls,
so N is made 0.02% or less. Preferably it is 0.017% or less.
[0052] When the steel sheet of the present invention contains C: 0.10 to 0.40% and Mn: 0.30
to 1.00%, embrittlement of the ferrite is suppressed, so N is made 0.01% or less.
Preferably it is 0.007% or less.
O: 0.02% or less
[0053] O is an element which, if present in a large amount, promotes the formation of coarse
oxides. For this reason, the smaller the amount of O, the better, but to lower O to
less than 0.0001%, the refining costs greatly increase, so the amount is made 0.0001%
or more. Preferably it is 0.0011% or more.
[0054] On the other hand, if over 0.020%, coarse oxides are formed in the steel, the oxides
become starting points of fracture at the time of cold forging, and the material formability
falls, so O is made 0.02% or less. Preferably it is 0.01% or less.
Sn: 0.05% or less
[0055] Sn is an element which unavoidably enters from the steel starting materials. For
this reason, the smaller the amount of Sn, the better. The content of S may also be
0, but to lower S to less than 0.001%, the refining costs greatly increase, so the
substantive lower limit is 0.001 to 0.002%.
[0056] On the other hand, if over 0.05%, the ferrite becomes brittle and the material formability
falls, so Sn is made 0.05% or less. Preferably it is 0.04% or less.
Sb: 0.05% or less
[0057] Sb, like Sn, is an element which unavoidably enters from the steel starting materials,
segregates at the ferrite grain boundaries, and reduces the number of carbides at
the ferrite grain boundaries. For this reason, the smaller the amount of Sb, the better.
The content of Sb may also be 0, but to lower Sb to less than 0.001%, the refining
costs greatly increase, so the substantive lower limit is 0.001 to 0.002%.
[0058] On the other hand, if over 0.050%, Sb segregates at the ferrite grain boundaries,
the number of carbides at the ferrite grain boundaries decreases, and the material
formability falls, so Sb is made 0.050% or less. Preferably it is 0.04% or less.
As: 0.05% or less
[0059] As, like Sn and Sb, is an element which unavoidably enters from the steel starting
materials and segregates at the ferrite grain boundaries. For this reason, the smaller
the amount of As, the better. The content of As may also be 0, but to lower As to
less than 0.001%, the refining costs greatly increase, so the substantive lower limit
is 0.001 to 0.002%.
[0060] On the other hand, if over 0.05%, As segregates at the ferrite grain boundaries,
the number of carbides at the ferrite grain boundaries decreases, and the material
formability falls, so As is made 50% or less. Preferably it is 0.04% or less.
[0061] The steel sheet of the present invention has the above elements as basic elements,
but may further contain the following elements for the purpose of improving the cold
forgeability of the steel sheet. The following elements are not essential for obtaining
the effects of the present invention, so the contents may also be 0.
Nb: 0.10% or less
[0062] Nb is an element effective for control of the form of the carbides. Further, it is
an element refining the structure and contributing to improvement of the toughness.
To obtain this effect of addition, Nb preferably is made 0.001% or more. More preferably
it is 0.002% or more.
[0063] On the other hand, if over 0.10%, a large number of fine Nb carbides precipitate,
the strength excessively rises, and, further, the number of carbides at the grain
boundaries falls and the cold forgeability falls, so Nb is made 0.10% or less. Preferably
it is 0.09% or less.
V: 0.10% or less
[0064] V, like Nb, is an element effective for control of the form of the carbides. Further,
it is an element refining the structure and contributing to improvement of the toughness.
To obtain this effect of addition, V preferably is made 0.01% or more. More preferably
it is 0.004% or more.
[0065] On the other hand, if over 0.10%, a large number of fine V carbides are formed, the
strength rises too much, the number of carbides at the ferrite grain boundaries decreases,
and the material formability falls, so V is made 0.10% or less. Preferably it is 0.09%
or less.
Cu: 0.10% or less
[0066] Cu is an element segregating at the ferrite grain boundaries. Further, it is an element
forming fine precipitates and contributing to the improvement of strength. To obtain
the effect of improvement of strength, Cu preferably is made 0.001% or more. More
preferably it is 0.008% or more.
[0067] On the other hand, if over 0.10%, segregation at the ferrite grain boundaries invites
red shortness and causes the productivity in hot rolling to fall, so Cu is made 0.10%
or less. Preferably it is 0.09% or less.
W: 0.10% or less
[0068] W, like Nb and V, is an element effective for control of the form of carbides. To
obtain this effect of addition, W preferably is made 0.001% or more. More preferably
it is 0.003% or more.
[0069] On the other hand, if over 0.10%, a large number of fine W carbides are formed, the
strength rises too much, the number of carbides at the ferrite grain boundaries decreases,
and the material formability falls, so W is made 0.10% or less. Preferably it is 0.08%
or less.
Ta: 0.001 to 0.10%
[0070] Ta, like Nb, V, and W, is an element effective for control of the form of carbides.
To obtain this effect of addition, Ta preferably is made 0.001% or more. More preferably
it is 0.007% or more.
[0071] On the other hand, if over 0.10%, a large number of fine Ta carbides are formed,
the strength rises too much, the number of carbides at the ferrite grain boundaries
decreases, and the material formability falls, so T is made 0.100% or less. Preferably
it is 0.09% or less.
Ni: 0.10% or less
[0072] Ni is an element effective for improvement of the impact resistance characteristic
of the formed part. To obtain this effect of addition, Ni preferably is made 0.001%
or more. More preferably it is 0.002% or more.
[0073] On the other hand, if over 0.10%, the number of carbides at the ferrite grain boundaries
decreases and the material formability falls, so Ni is made 0.10% or less. Preferably
it is 0.09% or less.
Mg: 0.05% or less
[0074] Mg is an element which can control the form of sulfides by addition in a trace amount.
To obtain this effect of addition, Mg preferably is made 0.0001% or more. More preferably
it is 0.0008% or more.
[0075] On the other hand, if over 0.05%, the ferrite becomes brittle and the material formability
falls, so Mg is made 0.05% or less. Preferably it is 0.04% or less.
Ca: 0.05% or less
[0076] Ca, like Mg, is an element which can control the form of sulfides by addition in
a trace amount. To obtain this effect of addition, Ca preferably is made 0.001% or
more. More preferably it is 0.003% or more.
[0077] On the other hand, if over 0.05%, coarse Ca oxides are formed and become starting
points of fracture at the time of forming by cold forging, that is, the material formability
falls, so Ca is made 0.05% or less. Preferably it is 0.04% or less.
Y: 0.05% or less
[0078] Y, like Mg and Ca, is an element which can control the form of sulfides by addition
in a trace amount. To obtain this effect of addition, Y preferably is made 0.001%
or more. More preferably it is 0.003% or more.
[0079] On the other hand, if over 0.05%, coarse Y oxides are formed and become starting
points of fracture at the time of forming by cold forging, that is, the material formability
falls, so Y is made 0.05% or less. Preferably it is 0.03% or less.
Zr: 0.05% or less
[0080] Zr, like Mg, Ca, and Y, is an element which can control the form of sulfides by addition
in a trace amount. To obtain this effect of addition, Zr preferably is made 0.001%
or more. More preferably it is 0.004% or more.
[0081] On the other hand, if over 0.05%, coarse Zr oxides are formed and become starting
points of fracture at the time of forming by cold forging, that is, the material formability
falls, so Zr is made 0.05% or less. Preferably it is 0.04% or less.
La: 0.05% or less
[0082] La is an element able to control the form of the sulfides by addition in a trace
amount, but is an element which segregates at the grain boundaries and reduces the
number of carbides at the ferrite grain boundaries. To obtain the effect of control
of the form of sulfides, La preferably is made 0.001% or more. More preferably it
is 0.003% or more.
[0083] On the other hand, if over 0.05%, La segregates at the ferrite grain boundaries,
the number of carbides at the ferrite grain boundaries decreases, and the material
formability falls, so La is made 0.05% or less. Preferably it is 0.04% or less.
Ce: 0.05% or less
[0084] Ce, like La, is an element able to control the form of the sulfides by addition in
a trace amount, but is an element which segregates at the grain boundaries and reduces
the number of carbides at the ferrite grain boundaries. To obtain the effect of control
of the form of sulfides, Ce preferably is made 0.001% or more. More preferably it
is 0.003% or more.
[0085] On the other hand, if over 0.05%, Ce segregates at the ferrite grain boundaries,
the number of carbides at the ferrite grain boundaries decreases, and the material
formability falls, so Ce is made 0.050% or less. Preferably it is 0.04% or less.
[0086] The balance of the chemical composition is Fe and unavoidable impurities.
[0087] Next, the structure of the steel sheet of the present invention will be explained.
[0088] The structure of the steel sheet of the present invention is a structure substantially
comprised of ferrite and carbides. Carbides are compounds of iron and carbon of cementite
(Fe
3C) plus compounds of cementite in which Fe atoms are substituted by Mn, Cr, and other
alloy elements and alloy carbides (M
23C
6, M
6C, MC, etc. [M: Fe and other metal elements added as alloys]).
[0089] When forming steel sheet into a predetermined part shape, a shear zone is formed
at the macrostructure of the steel sheet and slip deformation occurs concentrated
near the shear zone. In slip deformation, along with proliferation of dislocations,
a region of a high dislocation density is formed near the shear zone. Along with the
increase in the amount of strain imparted to the steel sheet, slip deformation is
promoted and the dislocation density increases.
[0090] In cold forging, strong working is performed with an equivalent strain exceeding
1. For this reason, in conventional steel sheet, it was not possible to prevent the
formation of voids and/or cracks along with the increase in dislocation density and
was difficult to improve the cold forgeability. To solve this problem, it is effective
to suppress the formation of a shear zone at the time of forming.
[0091] From the viewpoint of the microstructure, formation of a shear zone can be understood
as the phenomenon of slip occurring at a certain one grain crossing the crystal grain
boundary and being continuously propagated to the adjoining grain. Accordingly, to
suppress the formation of a shear zone, it is necessary to prevent propagation of
slip crossing crystal grain boundaries.
[0092] The carbides in steel sheet are strong particles inhibiting slip. By forming carbides
at the ferrite grain boundaries, it becomes possible to prevent the propagation of
slip crossing crystal grain boundaries and suppress the formation of a shear zone
and improve the cold forgeability. Simultaneously, the steel sheet is also improved
in formability.
[0093] The formability of steel sheet is largely due to the accumulation of strain inside
the crystal grains (accumulation of dislocations). If propagation of strain to the
adjoining crystal grains is blocked at the crystal grain boundaries, the amount of
strain inside the crystal grains increases. As a result, the work hardening rate increases
and the formability is improved.
[0094] To obtain such an effect, carbides have to be made to disperse in the metal structure
in suitable sizes. Therefore, the average grain size of carbides is made 0.4 µm to
2.0 µm. If the average grain size of the carbides is less than 0.4 µm, the steel sheet
remarkably increases in hardness and falls in cold forgeability. More preferably it
is 0.6 µm or more.
[0095] On the other hand, if the average particle size of the carbides exceeds 2.0 µm, at
the time of cold forming, the carbides form starting points of cracks. More preferably,
it is 1.95 µm or less.
[0096] Further, cementite, a carbide of iron, is a hard and brittle structure. If present
in the form of pearlite, which is a layered structure with ferrite, the steel becomes
hard and brittle. Therefore, pearlite has to be reduced as much as possible. In the
steel sheet of the present invention, the area ratio is made 6% or less.
[0097] Pearlite has a unique lamellar structure, so can be discerned by observation by an
SEM or optical microscope. By calculating the region of the lamellar structure at
any cross-section, the area ratio of the pearlite can be found.
[0098] Based on theory and principle, cold forgeability is considered to be strongly affected
by the rate of coverage of the ferrite grain boundaries by carbides. High precision
measurement is sought, but measurement of the rate of coverage of ferrite grain boundaries
by carbides in a three-dimensional space requires serial sectioning SEM observation
using an FIB to repeatedly cut a sample for observation in a scanning electron microscope
or 3D EBSP observation. A massive measurement time is required and technical knowhow
has to be built up.
[0099] The inventors judged that the above method of observation was not a general method
of analysis and did not employ it. They searched for a simpler, higher precision indicator
for evaluation. As a result, they discovered that it is possible to quantitatively
evaluate the cold forgeability and formability by using the ratio B/A of the number
B of carbides at the ferrite grain boundaries to the number A of carbides in the ferrite
grains as an indicator and that if the ratio B/A exceeds 1, the cold forgeability
and the formability in drawing and thickening remarkably rise.
[0100] Buckling, folding, and twisting of the steel sheet occurring at the time of cold
forging occur due to localization of strain accompanying the formation of a shear
zone, so by forming carbides at the ferrite grain boundaries, the formation of a shear
zone and localization of strain are reduced and buckling, folding, and twisting are
suppressed.
[0101] The carbides are observed by a scanning electron microscope. Before observation,
the sample for observation of the structure is polished by wet polishing by Emery
paper and a diamond abrasive having an average particle size of 1 µm, the observed
surface is polished to a mirror finish, then a 3% nitric acid-alcohol solution is
used to etch the structure. The magnification of the observation was made 3000X and
images of eight fields of 30 µm×40 µm at a sheet thickness 1/4 layer were captured
at random.
[0102] The obtained structural images were analyzed by image analyzing software (Win ROOF
made by Mitani Shoji) to measure in detail the areas of the carbides contained in
the analyzed regions. The circle equivalent diameters (=2×√(area/3.14)) were found
from the areas of the carbides and the average value was made the grain size of the
carbides. Note that, to keep down the effect of measurement error due to noise, carbides
with an area of 0.01 µm
2 or less are excluded from the coverage of the evaluation.
[0103] The number of carbides present at the ferrite grain boundaries are counted, the number
of carbides at the grain boundaries are subtracted from the total number of carbides,
and the number of carbides in the ferrite grains are found. Based on the measured
and calculated number of carbides, the ratio B/A of the number B of carbides at the
ferrite grain boundaries with respect to the number A of carbides inside the ferrite
grains is calculated.
[0104] In the structure of the steel sheet after annealing, the ferrite grain size is preferably
3 µm to 50 µm from the viewpoint of improvement of the cold forgeability. If the ferrite
grain size is less than 3 µm, the hardness increases and fractures and cracks easily
form at the time of cold forging, so the ferrite grain size is preferably 3 µm or
more. More preferably it is 5 µm or more.
[0105] If the ferrite grain size is over 50.0 µm, the number of carbides on the crystal
grain boundaries suppressing the propagation of slip is decreased and the cold forgeability
falls, so the ferrite grain size is preferably 50 µm or less. More preferably it is
40 µm or less.
[0106] The ferrite grain size is measured by using the above-mentioned procedure to polish
the observed surface of the sample surface to a mirror finish, then etching it by
a 3% nitric acid-alcohol solution and observing the structure by an optical microscope
or scanning electron microscope and applying the line segment method to the captured
image.
[0107] At the time of cold forging, in addition to control of the form of carbides, drawability
at the time of cold forging becomes necessary.
[0108] To improve the drawability at the time of cold forging, improvement of the plastic
anisotropy becomes necessary. For this reason, control of the texture at the hot rolled
steel sheet is necessary. The texture is evaluated by X-ray diffraction at a plane
parallel to the sheet surface at a 1/2 sheet thickness part of the hot rolled steel
sheet. For X-ray diffraction, X-rays from a Mo tube are used.
[0109] The diffraction intensities at the diffraction orientations {110}, {220}, {211},
and {310} due to reflection are obtained and based on these an ODF is prepared. For
the preparation of the ODF, the diffraction intensity data of random orientations
of iron is used. From this, the X-ray diffraction intensity of {211}<011> is found
as I1 and the X-ray diffraction intensity of {100}<011> is found as I0. If this I1/I0
is less than 1, it means that the recrystallization necessary for a random texture
appears at the time of hot rolling. If the random texture can be obtained, the plastic
anisotropy is reduced and the formability is improved.
[0110] By making the Vickers hardness of the steel sheet 100 HV to 150 HV (when C: 0.10
to 0.40% and Mn: 0.01 to 0.30%) or by making it 100 HV to 170 HV, it is possible to
improve the formability at the time of cold forging. If the Vickers hardness is less
than 100 HV, buckling easily occurs during the forming at the time of cold forging
and the shaped part falls in precision, so the Vickers hardness is made 100 HV or
more. Preferably, it is 110 HV or more.
[0111] If the Vickers hardness is over 170HV, the ductility falls, buckling to outside the
plane easily occurs during thickening or other compression deformation, further, internal
fracture easily occurs at the time of cold forging, and the impact resistance characteristic
deteriorates, so the Vickers hardness is made 170 HV or less. To reliably secure the
ductility and impact resistance characteristic, the Vickers hardness is preferably
made 150 HV or less. More preferably, it is 140HV or less.
[0112] Next, the method of production of steel sheet of the present invention will be explained.
[0113] The method of production of the present invention has as its basic idea to use a
steel slab of the above-mentioned chemical composition and integrally manage the hot
rolling conditions and annealing conditions to control the structure of the steel
sheet.
[0114] First, a steel slab obtained by continuously casting molten steel of the required
chemical composition is used for hot rolling. The continuously cast slab may be directly
used for hot rolling or may be used for hot rolling after cooling once, then heating.
[0115] If cooling once, then heating the steel slab for use for hot rolling, the heating
temperature is preferably 1000°C to 1250°C and the heating time is preferably 0.5
hour to 3 hours. If directly using the continuously cast steel slab for hot rolling,
the temperature of the steel slab used for the hot rolling is preferably made 1000°C
to 1250°C.
[0116] If the temperature of the steel slab or the heating temperature of the steel slab
is over 1250°C or the heating time of the steel slab is over 3 hours, decarburization
from the surface layer of the steel slab becomes remarkable, at the time of heating
before carburization and quenching, the austenite grains at the surface layer of the
steel sheet abnormally grow, and the impact resistance falls. For this reason, the
temperature of the steel slab or the heating temperature of the steel slab is preferably
1250°C or less and the heating time is preferably 3 hours or less. More preferably,
they are 1200°C or less and 2.5 hours or less.
[0117] If the temperature of the steel slab or the heating temperature of the steel slab
is less than 1000°C or the heating time is less than 0.5 hour, the microsegregation
and macrosegregation occurring in casting cannot be eliminated, regions remain inside
the steel slab where Si, Mn, and other alloy elements locally concentrate, and the
impact resistance falls. For this reason, the temperature of the steel slab or the
heating temperature of the steel slab is preferably 1000°C or more and the heating
time is preferably 0.5 hour or more. More preferably they are 1050°C or more and 1
hour or more.
[0118] The finish rolling in the hot rolling is completed at 820°C or more, preferably at
900°C to 950°C in temperature region. If the finish rolling temperature is less than
820°C, the steel sheet increases in deformation resistance, the rolling load remarkably
rises, and, further, the amount of roll wear increases and the productivity falls.
Along with this, the recrystallization required for improving the plastic anisotropy
does not sufficiently proceed, so the finish rolling temperature is made 820°C or
more. From the viewpoint of promoting recrystallization, it is preferably 900°C or
more.
[0119] If the finish rolling temperature is over 950°C, bulky scale forms during passage
through the run out table (ROT). Due to this scale, flaws are formed at the surface
of the steel sheet. When an impact load is applied after cold forging and carburization,
quenching, and tempering, cracks easily form starting from the flaws, so the steel
sheet falls in impact resistance. For this reason, the finish rolling temperature
is made 950°C or less. Preferably it is 920°C or less.
[0120] When cooling the hot rolled steel sheet after finish rolling at the ROT, the cooling
rate is preferably 10°C/sec to 100°C/sec. If the cooling rate is less than 10°C/sec,
bulky scale is formed during the cooling. It is not possible to suppress the formation
of flaws due to this and the impact resistance falls, so the cooling rate is preferably
10°C/sec or more. More preferably it is 15°C/sec or more.
[0121] If cooling from the surface layer of the steel sheet to the inside by an over 100°C/sec
cooling rate, the outermost layer part is excessively heated and bainite, martensite,
and other low temperature transformed structures are formed. When coiling, then cooling
down to 100°C to room temperature, then paying out the hot rolled steel sheet coil,
microcracks form in the low temperature transformed structures. The microcracks are
difficult to remove by pickling and cold rolling.
[0122] Further, if applying an impact load to the steel sheet after cold forging and carburization,
quenching, and tempering, cracks advance starting from the microcracks, so the impact
resistance falls. For this reason, to suppress the formation of bainite, martensite,
and other low temperature transformed structures at the outermost layer part of the
steel sheet, the cooling rate is preferably 100°C/sec or less. More preferably it
is 90°C/sec or less.
[0123] Note that, the cooling rate indicates the cooling ability received from the cooling
facilities in a water spray section at the time when being cooled on the ROT down
to the target temperature of coiling from the time when the hot rolled steel sheet
after finish rolling is water cooled at a water spray section after passing through
a non-water spray section. It does not show the average cooling rate from the starting
point of water spray to the temperature at which the steel sheet is coiled up by the
coiler.
[0124] The coiling temperature is made 400°C to 550°C. This is a temperature lower than
the general coiling temperature and in particular is a condition not generally used
when the content of C is high. By coiling up the hot rolled steel sheet produced under
the above conditions in this temperature range, the structure of the steel sheet can
be made a bainite structure comprised of fine ferrite in which carbides are dispersed.
[0125] If the coiling temperature is less than 400°C, the austenite, which was not transformed
before coiling, transforms to hard martensite. At the time of paying out the hot rolled
steel sheet coil, cracks form at the surface layer of the hot rolled steel sheet and
the impact resistance falls.
[0126] Furthermore, at the time of recrystallization from austenite to ferrite, since the
recrystallization driving force is small, the recrystallized ferrite grains are strongly
influenced in orientation by the orientation of the austenite grains and randomization
of the texture becomes difficult. For this reason, the coiling temperature is made
400°C or more. Preferably it is 430°C or more.
[0127] If the coiling temperature is over 550°C, pearlite with the large lamellar spacing
is formed and highly heat stable bulky needle-shaped carbides are formed. These needle-shaped
carbides remain even after two-stage annealing. At the time of cold forging and otherwise
forming steel sheet, cracks are formed starting from these needle-shaped carbides.
[0128] Further, at the time of recrystallization from austenite to ferrite, conversely the
recrystallization driving force becomes too large. In this case as well, the result
becomes recrystallized ferrite grains heavily dependent on the orientation of the
austenite grains and the texture is not randomized. For this reason, the coiling temperature
is made 550°C or less. Preferably it is 520°C or less.
[0129] The hot rolled steel sheet coil is paid out and pickled, then is held in two temperature
regions for two-stage step type of annealing (two-stage annealing). By treating the
hot rolled steel sheet by two-stage annealing, the stability of the carbides is controlled
to promote the formation of carbides at the ferrite grain boundaries.
[0130] If cold rolling the pickled steel sheet before annealing treatment, the ferrite grains
are refined, so the steel sheet becomes harder to soften. For this reason, in the
present invention, it is not preferable to cold roll the steel before annealing. It
is preferable to perform the annealing treatment without cold rolling after the pickling.
[0131] The first stage of annealing is performed at 650 to 720°C, preferably the A
c1 point or less in temperature region. Due to this annealing, the carbides are coarsened
and partially spheroidized and the alloy elements are made to concentrate at the carbides
to thereby raise the thermal stability of the carbides.
[0132] In the first stage of annealing, the heating rate up to the annealing temperature
(below, referred to as the "first stage heating rate") is made 30°C/hour to 150°C/hour.
If the first stage heating rate is less than 30°C/hour, raising the temperature takes
time and the productivity falls, so the first stage heating rate is made 3°C/hour
or more. Preferably it is 10°C/hour or more.
[0133] On the other hand, if the first stage heating rate is over 150°C/hour, the temperature
difference between the outer circumferential part and the inside part of the hot rolled
steel sheet coil increases, scratches and seizing occur due to the difference in heat
expansion, and relief shapes are formed at the steel sheet surface. At the time of
cold forging and other forming, cracks occur starting from the relief shapes and result
in a drop in cold forgeability and a drop in formability and impact resistance after
carburizing, quenching, and tempering, so the first stage heating rate is made 150°C/hour
or less. Preferably, it is 130°C/hour or less.
[0134] The annealing temperature in the first stage of annealing (below, referred to as
"the first stage annealing temperature") is made 650°C to 720°C. If the first stage
annealing temperature is less than 650°C, the carbides become insufficient in stability
and it becomes difficult to form carbides remaining in the austenite in the second
stage of annealing. Therefore, the first stage annealing temperature is made 650°C
or more. Preferably it is 670°C or more.
[0135] On the other hand, if the annealing temperature exceeds 720°C, before the carbides
rise in stability, austenite is formed and it becomes impossible to control the above-mentioned
changes in structure, so the first stage annealing temperature is made 720°C or less.
Preferably it is 700°C or less.
[0136] The annealing time in the first stage of annealing (below, referred to as the "first
stage annealing time") is made 3 hours to 60 hours. If the first stage annealing time
is less than 3 hours, the carbides become insufficient in stability and it becomes
difficult to form carbides remaining in the second stage of annealing. Therefore,
the first stage annealing time is made 3 hours or more. Preferably it is 5 hours or
more.
[0137] On the other hand, if the first stage annealing time exceeds 60 hours, no further
stabilization of the carbides can be expected. Furthermore, the productivity drops.
Therefore, the first stage annealing time is made 60 hours or less. Preferably it
is 55 hours or less.
[0138] After that, the temperature is raised to 725 to 790°C, preferably the A
c1 point to the A
3 point in temperature region, to form austenite in the structure. At this time, the
carbides in the fine ferrite grains dissolve in the austenite, but the carbides coarsened
due to the first stage of annealing remain in the austenite.
[0139] When cooling without performing the second stage of annealing, the ferrite grain
size does not become larger and the ideal structure cannot be obtained.
[0140] The heating rate up to the annealing temperature in the second stage of annealing
(below, referred to as the "second stage heating rate") is made 1°C/hour to 80°C/hour.
At the time of the second stage of annealing, austenite is formed and grows from the
ferrite grain boundaries. At that time, by slowing the heating rate up to the annealing
temperature, it becomes possible to suppress the formation of nuclei of austenite
raise the rate of coverage of the grain boundaries by carbides in the structure formed
by gradual cooling after annealing.
[0141] For this reason, the second stage heating rate preferably is slow, but if less than
1°C/hour, raising the temperature takes time and the productivity falls, so the second
stage heating rate is made 1°C/hour or more. Preferably it is 10°C/hour or more.
[0142] If the second stage heating rate is over 80°C/hour, the temperature difference between
the outer circumferential part and the inside part of the hot rolled steel sheet coil
increases, scratches and seizing occur due to the large difference in heat expansion
due to the transformation, and relief shapes are formed at the steel sheet surface.
At the time of cold forging, cracks occur starting from the relief shapes and result
in a drop in cold forgeability and formability and further a drop in the impact resistance
after carburizing, quenching, and tempering as well, so the second stage heating rate
is made 80°C/hour or less. Preferably, it is 70°C/hour or less.
[0143] The annealing temperature in the second stage of annealing (below, referred to as
"the second stage annealing temperature") is made 725°C to 790°C. If the second stage
annealing temperature is less than 725°C, the amount of austenite formed becomes smaller,
the number of carbides at the ferrite grain boundaries decreases after cooling after
the second stage of annealing, and, further, the ferrite grain size becomes smaller.
Therefore, the second stage annealing temperature is made 725°C or more. Preferably
it is 735°C or more.
[0144] On the other hand, if the second stage annealing temperature exceeds 790°C, it becomes
difficult to make carbides remain in the austenite and it becomes difficult to control
the changes in structure, so the second stage annealing temperature is made 790°C
or less. Preferably it is 770°C or less.
[0145] The annealing time in the second stage of annealing ("second stage annealing time")
is made 3 hours to 10 hours. If the second stage annealing time is less than 3 hours,
the amount of formation of austenite becomes small, the carbides inside the ferrite
grains do not sufficiently dissolve, it becomes difficult to make the number of carbides
at the ferrite grain boundaries increase, and, further, the ferrite grain size becomes
small. Therefore, the second stage annealing time is made 3 hours or more. Preferably
it is 5 hours or more.
[0146] On the other hand, if the second stage annealing time exceeds 10 hours, it becomes
difficult to make carbides remain in the austenite. Further, the manufacturing costs
also increase. Therefore, the second stage annealing time is made less than 10 hours.
Preferably it is 8 hours or less.
[0147] After the two-stage annealing, the steel sheet is cooled by a 1°C/ hour to 100°C/hour
cooling rate down to 650°C.
[0148] By gradually cooling the austenite formed at the second stage of annealing due to
gradual cooling, it transforms to ferrite, carbon atoms are adsorbed at the carbides
remaining in the austenite, the carbides and austenite cover the ferrite grain boundaries,
and, finally, a structure can be obtained in which a large amount of carbides are
present at the ferrite grain boundaries. For this reason, the cooling rate is preferably
slow, but if less than 1°C/hour, the time required for cooling increases and the productivity
falls, so the cooling rate is made 1°C/hour or more. Preferably it is 10°C/hour or
more.
[0149] On the other hand, if the cooling rate is over 100°C/hour, the austenite transforms
to pearlite, the steel sheet increases in hardness, and the cold forgeability falls.
Further, after carburization, quenching, and tempering, the impact resistance falls.
Therefore, the cooling rate is made 100°C/hour or less. Preferably it is 80°C/hour
or less.
[0150] Furthermore, after cooling it down to 650°C, the steel sheet is cooled down to room
temperature. The cooling rate at this time is not limited.
[0151] The atmosphere in the two-stage annealing is not particularly limited. For example,
it may be any of a 95% or more nitrogen atmosphere, 95% or more hydrogen atmosphere,
or air atmosphere.
[0152] As explained above, according to the method of production of the present invention
integrally managing the hot rolling conditions and annealing conditions and controlling
the structure of the steel sheet, it is possible to produce steel sheet excellent
in formability at the time of cold forging combining drawing and thickening and, furthermore,
excellent in the hardenability required for improvement of the impact resistance after
carburization, quenching, and tempering. Examples
[0153] Next, examples of the present invention will be explained, but the conditions in
the examples are illustrations of conditions employed for confirming the workability
and effects of the present invention. The present invention is not limited to these
illustrations of conditions. The present invention can employ various conditions so
long as not departing from the gist of the present invention and achieving the object
of the present invention.
Example 1
[0154] A continuously cast slab (steel slab) of each of the chemical compositions shown
in Table 1 and Table 2 (continuation of Table 1) was heated at 1240°C for 1.8 hours,
then hot rolled, cooled down to 530°C by a 45°C/sec cooling rate on the ROT after
finish hot rolling at 920°C, and coiled at 520°C to produce sheet thickness 5.2 mm
hot rolled steel sheet coil.
[0155] The hot rolled steel sheet coil was paid out and pickled, then was loaded into a
box type annealing furnace. The annealing atmosphere was controlled to 95% hydrogen
-5% nitrogen, then the coil was heated from room temperature to 705°C by a 100°C/hour
heating rate and was held at 710°C for 24 hours to obtain a uniform temperature distribution
inside the hot rolled steel sheet coil.
[0156] Next, the coil was heated by a 5°C/hour heating rate to 740°C, was further held at
740°C for 5 hours, then was cooled down to 650°C by a 10°C/hour cooling rate, then
was furnace cooled down to room temperature to prepare a sample for evaluation of
performance. The structure of the sample was observed by the method explained above
and the ferrite grain size and number of carbides were measured.
Table 1
| No |
C |
Si |
Mn |
P |
S |
Al |
N |
O |
Ti |
Cr |
Mo |
B |
Nb |
V |
Cu |
Remarks |
| 1 |
0.35 |
0.21 |
0.53 |
0.0105 |
0.0027 |
0.065 |
0.0067 |
0.01 |
0.041 |
0.0300 |
0.1760 |
0.0090 |
|
|
|
Inv.steel |
| 2 |
0.24 |
0.22 |
0.59 |
0.0075 |
0.0040 |
0.066 |
0.0021 |
0.01 |
0.035 |
0.4500 |
0.1330 |
0.0055 |
|
|
|
Inv.steel |
| 3 |
0.18 |
0.03 |
0.41 |
0.0165 |
0.0026 |
0.029 |
0.0050 |
0.01 |
0.094 |
0.1500 |
0.4390 |
0.0022 |
|
|
|
Inv.steel |
| 4 |
0.31 |
0.13 |
0.31 |
0.0003 |
0.0053 |
0.072 |
0.0048 |
0.02 |
0.050 |
0.1300 |
0.2510 |
0.0028 |
|
|
|
Inv.steel |
| 5 |
0.25 |
0.09 |
0.39 |
0.0021 |
0.0088 |
0.055 |
0.0079 |
0.01 |
0.085 |
0.0500 |
0.3580 |
0.0098 |
|
|
|
Inv.steel |
| 6 |
0.13 |
0.04 |
0.7 |
0.0088 |
0.0066 |
0.072 |
0.0031 |
0.02 |
0.058 |
0.4900 |
0.0170 |
0.0018 |
|
|
|
Inv.steel |
| 7 |
0.14 |
0.04 |
0.32 |
0.0133 |
0.0081 |
0.052 |
0.0017 |
0.02 |
0.094 |
0.3700 |
0.3190 |
0.0093 |
|
|
|
Inv.steel |
| 8 |
0.21 |
0.03 |
0.93 |
0.0147 |
0.0077 |
0.074 |
0.0021 |
0.01 |
0.085 |
0.3300 |
0.1440 |
0.0042 |
|
|
|
Inv.steel |
| 9 |
0.29 |
0.22 |
0.4 |
0.0118 |
0.0082 |
0.036 |
0.0071 |
0.01 |
0.040 |
0.2700 |
0.0170 |
0.0082 |
|
|
|
Inv.steel |
| 10 |
0.31 |
0.23 |
0.6 |
0.0040 |
0.0068 |
0.037 |
0.0010 |
0.01 |
0.039 |
0.2400 |
0.4480 |
0.0020 |
|
|
|
Inv.steel |
| 11 |
1.20 |
0.02 |
0.78 |
0.0176 |
0.0049 |
0.073 |
0.0092 |
0.00 |
0.020 |
0.1600 |
0.0070 |
0.0024 |
|
|
|
Comp.steel |
| 12 |
0.27 |
1.50 |
1.0 |
0.0170 |
0.0029 |
0.013 |
0.0004 |
0.00 |
0.037 |
0.2900 |
0.2990 |
0.0096 |
|
|
|
Comp.steel |
| 13 |
0.37 |
0.21 |
3.3 |
0.0189 |
0.0052 |
0.046 |
0.0099 |
0.01 |
0.027 |
0.1400 |
0.2770 |
0.0077 |
|
|
|
Comp.steel |
| 14 |
0.39 |
0.27 |
0.83 |
0.0091 |
0.0059 |
0.018 |
0.0023 |
0.01 |
0.038 |
1.1000 |
0.4070 |
0.0099 |
|
|
|
Comp.steel |
| 15 |
0.35 |
0.26 |
0.37 |
0.0143 |
0.0031 |
0.018 |
0.0063 |
0.00 |
0.028 |
0.0200 |
0.1340 |
0.0000 |
|
|
|
Comp.steel |
| 16 |
0.22 |
0.05 |
0.36 |
0.0109 |
0.0032 |
0.067 |
0.0008 |
0.0062 |
0.001 |
0.18 |
0.081 |
0.0014 |
0.028 |
0.083 |
|
Inv.steel |
| 17 |
0.35 |
0.2 |
0.47 |
0.0137 |
0.0004 |
0.052 |
0.0013 |
0.0127 |
0.054 |
0.45 |
0.241 |
0.0057 |
|
|
|
Inv.steel |
| 18 |
0.37 |
0.07 |
0.95 |
0.0076 |
0.0008 |
0.057 |
0.0098 |
0.0149 |
0.097 |
0.23 |
0.074 |
0.0019 |
|
|
|
Inv.steel |
| 19 |
0.37 |
0.23 |
0.76 |
0.0086 |
0.0058 |
0.073 |
0.0057 |
0.0076 |
0.076 |
0. 18 |
0.149 |
0.0007 |
|
|
|
Inv.steel |
| 20 |
0.32 |
0.17 |
0.61 |
0.0197 |
0.0024 |
0.011 |
0.0009 |
0.0153 |
0.083 |
0.27 |
0.295 |
0.0019 |
|
|
|
Inv.steel |
| 21 |
0.22 |
0.27 |
0.57 |
0.0059 |
0.0013 |
0.048 |
0.0041 |
0.0064 |
0.005 |
0.33 |
0.438 |
0.0085 |
|
|
|
Inv.steel |
| 22 |
0.12 |
0.19 |
0.32 |
0.0135 |
0.0032 |
0.078 |
0.0096 |
0.0107 |
0.083 |
0.06 |
0.167 |
0.0051 |
|
|
0.024 |
Inv.steel |
| 23 |
0.25 |
0.13 |
0.8 |
0.0056 |
0.0046 |
0.087 |
0.0064 |
0.0001 |
0.04 |
0.32 |
0.33 |
0.0079 |
|
|
|
Inv.steel |
| 24 |
0.31 |
0.16 |
0.41 |
0.0142 |
0.0097 |
0.026 |
0.0054 |
0.0081 |
0.003 |
0.14 |
0.473 |
0.0049 |
|
|
|
Inv.steel |
| 25 |
0.22 |
0.23 |
0.42 |
0.0052 |
0.003 |
0.093 |
0.0055 |
0.0197 |
0.05 |
0.21 |
0.349 |
0.0081 |
|
|
|
Inv.steel |
| 26 |
0.34 |
0.24 |
0.68 |
0.01 |
0.0081 |
0.024 |
0.0077 |
0.0092 |
0.085 |
0.05 |
0.212 |
0.0024 |
0.044 |
0.09 |
|
Comp.steel |
| 27 |
0.11 |
0.09 |
0.45 |
0.0124 |
0.0068 |
0.008 |
0.0059 |
0.0151 |
0.044 |
0.41 |
0.109 |
0.0074 |
|
|
0.21 |
Comp. steel |
| 28 |
0.2 |
0.28 |
0.5 |
0.0196 |
0.0007 |
0.003 |
0.0060 |
0.0137 |
0.012 |
0.3 |
0.406 |
0.0013 |
|
|
|
Comp.steel |
| 29 |
0.34 |
0.1 |
0.71 |
0.0004 |
0.003 |
0.014 |
0.0059 |
0.0093 |
0.092 |
0.02 |
0.189 |
0.0082 |
|
0.22 |
0.004 |
Comp.steel |
| 30 |
0.37 |
0.09 |
0.8 |
0.007 |
0.0071 |
0.043 |
0.0032 |
0.0023 |
0.016 |
0.33 |
0.253 |
0.0044 |
0.36 |
|
|
Comp.steel |
| 31 |
0.33 |
0.21 |
0.53 |
0.0104 |
0.0028 |
0.066 |
0.0069 |
0.01 |
0.039 |
0.0320 |
0.1730 |
0.0093 |
|
|
|
Inv.steel |
| 32 |
0.36 |
0.04 |
0.32 |
0.011 |
0.0032 |
0.067 |
0.0008 |
0.0062 |
0.001 |
0.18 |
0.081 |
0.0014 |
0.054 |
0.087 |
|
Inv.steel |
| 33 |
0.34 |
0.20 |
1.21 |
0.0105 |
0.0027 |
0.065 |
0.0075 |
0.01 |
0.041 |
0.0320 |
0.1720 |
0.0095 |
|
|
|
Inv.steel |
| 34 |
0.22 |
0.05 |
1.83 |
0.01 |
0.0032 |
0.066 |
0.0007 |
0.0062 |
0.001 |
0.18 |
0.081 |
0.0014 |
0.032 |
0.096 |
|
Inv.steel |
| 35 |
0.37 |
0.21 |
1.3 |
0.0104 |
0.0029 |
0.065 |
0.0063 |
0.01 |
0.038 |
0.0280 |
0.1690 |
0.0096 |
|
|
|
Inv.steel |
| 36 |
0.22 |
0.06 |
2.19 |
0.0109 |
0.0035 |
0.067 |
0.0008 |
0.0062 |
0.001 |
0.18 |
0.081 |
0.0014 |
0.036 |
0.065 |
|
Inv.steel |
Table 2 (Continuation of Table 1) (mass%)
| No |
W |
Ta |
Ni |
Sn |
Sb |
As |
Mg |
Ca |
Y |
Zr |
La |
Ce |
Remarks |
| 1 |
|
|
|
|
|
|
|
|
|
|
|
|
Inv.steel |
| 2 |
|
|
|
|
|
|
|
|
|
|
|
|
Inv.steel |
| 3 |
|
|
|
|
|
|
|
|
|
|
|
|
Inv.steel |
| 4 |
|
|
|
|
|
|
|
|
|
|
|
|
Inv.steel |
| 5 |
|
|
|
|
|
|
|
|
|
|
|
|
Inv.steel |
| 6 |
|
|
|
|
|
|
|
|
|
|
|
|
Inv.steel |
| 7 |
|
|
|
|
|
|
|
|
|
|
|
|
Inv.steel |
| 8 |
|
|
|
|
|
|
|
|
|
|
|
|
Inv.steel |
| 9 |
|
|
|
|
|
|
|
|
|
|
|
|
Inv.steel |
| 10 |
|
|
|
|
|
|
|
|
|
|
|
|
Inv.steel |
| 11 |
|
|
|
|
|
|
|
|
|
|
|
|
Comp. steel |
| 12 |
|
|
|
|
|
|
|
|
|
|
|
|
Comp.steel |
| 13 |
|
|
|
|
|
|
|
|
|
|
|
|
Comp.steel |
| 14 |
|
|
|
|
|
|
|
|
|
|
|
|
Comp.steel |
| 15 |
|
|
|
|
|
|
|
|
|
|
|
|
Comp. steel |
| 16 |
|
|
|
|
|
|
|
|
|
|
|
|
Inv.steel |
| 17 |
|
0.033 |
|
0.043 |
|
|
|
|
|
|
|
|
Inv.steel |
| 18 |
0.091 |
|
|
|
|
|
|
|
|
|
|
|
Inv.steel |
| 19 |
|
|
|
|
0.014 |
|
|
|
|
|
|
|
Inv.steel |
| 20 |
|
|
|
|
|
0.032 |
|
|
0.022 |
|
|
|
Inv.steel |
| 21 |
|
|
|
|
|
|
0.0424 |
|
|
|
|
|
Inv.steel |
| 22 |
|
|
|
|
|
0.031 |
|
|
|
|
|
0.046 |
Inv.steel |
| 23 |
|
|
|
|
|
|
|
|
|
|
0.046 |
|
Inv.steel |
| 24 |
|
|
0.017 |
|
|
|
|
|
|
0.024 |
|
|
Inv.steel |
| 25 |
|
|
|
|
|
|
|
0.027 |
|
|
|
|
Inv.steel |
| 26 |
|
|
0.15 |
|
|
|
|
|
|
|
|
|
Comp.steel |
| 27 |
|
0.049 |
|
|
|
|
|
0.05 |
|
|
|
|
Comp.steel |
| 28 |
0.33 |
|
|
0.012 |
|
|
|
|
|
0.041 |
|
|
Comp. steel |
| 29 |
|
|
|
|
|
|
|
|
0.024 |
|
|
|
Comp.steel |
| 30 |
|
|
|
|
|
|
|
|
|
|
0.002 |
|
Comp.steel |
| 31 |
|
|
|
|
|
|
|
|
|
|
|
|
Inv.steel |
| 32 |
|
|
|
|
|
|
|
|
|
|
|
|
Inv.steel |
| 33 |
|
|
|
|
|
|
|
|
|
|
|
|
Inv.steel |
| 34 |
|
|
|
|
|
|
|
|
|
|
|
|
Inv.steel |
| 35 |
|
|
|
|
|
|
|
|
|
|
|
|
Inv.steel |
| 36 |
|
|
|
|
|
|
|
|
|
|
|
|
Inv.steel |
[0157] Table 3 shows the ferrite grain size (µm), average carbide grain size (µm), pearlite
area ratio (%), Vickers hardness (HV), number of grain boundary carbides/number of
grain carbides, X-ray intensity ratio I1/I0, "r" value anisotropy index |Δr|, and
critical cooling rate (°C/sec) shown in Table 1 and Table 2. If I1/I0 is 1 or more,
the recrystallization in hot rolling does not sufficiently proceed and the steel sheet
becomes larger in plastic anisotropy. Note that, the "r" value anisotropy index |Δr|
was found by a tensile test
Table 3
| No |
Ferrite grain size (µm) |
Average carbide grain size (µm) |
Pearlite area rate (%) |
Vickers hardness (HV) |
No. of grain boundary carbides/No. of grain carbides |
I1/I0 |
|Δr| |
Critical cooling rate (°C/sec) |
Remarks |
| 1 |
17 |
0.7 |
1.7 |
120 |
5.66 |
0.75 |
0.17 |
29.8 |
Inv.ex. |
| 2 |
23 |
1.1 |
1.2 |
118 |
5.85 |
0.81 |
0.19 |
29.8 |
Inv.ex. |
| 3 |
16 |
0.8 |
0.8 |
105 |
3.88 |
0.80 |
0.18 |
29.9 |
Inv.ex. |
| 4 |
13 |
1.1 |
1.3 |
109 |
5.54 |
0.76 |
0.17 |
30.0 |
Inv.ex. |
| 5 |
20 |
0.9 |
1.0 |
108 |
3.48 |
0.69 |
0.15 |
29.9 |
Inv.ex. |
| 6 |
12 |
1.1 |
0.0 |
115 |
7.11 |
0.67 |
0.14 |
29.9 |
Inv.ex. |
| 7 |
13 |
1.3 |
1.0 |
100 |
6.11 |
0.64 |
0.13 |
30.1 |
Inv.ex. |
| 8 |
11 |
1.2 |
1.3 |
124 |
4.23 |
0.64 |
0.13 |
29.7 |
Inv.ex. |
| 9 |
20 |
1.1 |
1.2 |
113 |
6.07 |
0.79 |
0.18 |
29.9 |
Inv.ex. |
| 10 |
17 |
1.4 |
1.9 |
122 |
6.59 |
0.65 |
0.13 |
29.8 |
Inv.ex. |
| 11 |
18 |
1.1 |
9.1 |
167 |
5.36 |
0.69 |
0.15 |
30.0 |
Comp.ex. |
| 12 |
10 |
1.0 |
1.5 |
154 |
6.86 |
0.69 |
0.15 |
29.4 |
Comp.ex. |
| 13 |
14 |
1.3 |
12.3 |
178 |
5.69 |
0.72 |
0.16 |
13.2 |
Comp.ex. |
| 14 |
20 |
1.0 |
1.2 |
133 |
0.91 |
0.78 |
0.18 |
29.6 |
Comp.ex. |
| 15 |
12 |
1.1 |
1.9 |
114 |
6.04 |
0.79 |
0.18 |
311.0 |
Comp.ex. |
| 16 |
11 |
0.8 |
1.8 |
105 |
5.02 |
0.63 |
0.13 |
30.1 |
Inv.ex. |
| 17 |
26 |
1.0 |
1.6 |
119 |
4.19 |
0.66 |
0.14 |
29.8 |
Inv.ex. |
| 18 |
13 |
1.2 |
1.0 |
134 |
5.05 |
0.78 |
0.18 |
29.6 |
Inv.ex. |
| 19 |
11 |
1.2 |
1.8 |
130 |
5.36 |
0.75 |
0.17 |
29.6 |
Inv.ex. |
| 20 |
20 |
1.1 |
1.0 |
122 |
4.17 |
0.65 |
0.13 |
29.7 |
Inv.ex. |
| 21 |
11 |
1.1 |
1.0 |
116 |
5.57 |
0.74 |
0.16 |
29.9 |
Inv.ex. |
| 22 |
17 |
1.1 |
0.6 |
100 |
6.17 |
0.82 |
0.19 |
30.1 |
Inv.ex. |
| 23 |
14 |
1.2 |
1.0 |
122 |
6.19 |
0.77 |
0.17 |
29.7 |
Inv.ex. |
| 24 |
12 |
1.1 |
1.8 |
113 |
7.12 |
0.81 |
0.19 |
29.9 |
Inv.ex. |
| 25 |
17 |
0.8 |
1.4 |
111 |
5.38 |
0.74 |
0.16 |
29.9 |
Inv.ex. |
| 26 |
13 |
1.2 |
1.4 |
126 |
6.46 |
0.80 |
0.18 |
29.6 |
Comp.ex. |
| 27 |
19 |
1.1 |
1.2 |
105 |
6.93 |
0.74 |
0.16 |
30.0 |
Comp.ex. |
| 28 |
23 |
0.9 |
1.8 |
113 |
6.58 |
0.70 |
0.15 |
29.9 |
Comp.ex. |
| 29 |
18 |
1.2 |
0.5 |
125 |
4.62 |
0.71 |
0.15 |
29.7 |
Comp.ex. |
| 30 |
14 |
1.1 |
0.7 |
129 |
4.93 |
0.68 |
0.14 |
29.7 |
Comp.ex. |
| 31 |
18 |
1.1 |
1.5 |
125 |
5.72 |
0.75 |
0.17 |
29.3 |
Inv.ex. |
| 32 |
13 |
0.8 |
0.2 |
109 |
5.17 |
0.63 |
0.13 |
29.7 |
Inv.ex. |
| 33 |
18 |
1.3 |
1.2 |
125 |
5.60 |
0.75 |
0.16 |
31.2 |
Inv.ex. |
| 34 |
13 |
1.4 |
1.9 |
109 |
4.97 |
0.63 |
0.13 |
30.9 |
Inv.ex. |
| 35 |
18 |
1.3 |
1.4 |
128 |
5.75 |
0.75 |
0.17 |
29.5 |
Inv.ex. |
| 36 |
13 |
1.4 |
1.0 |
110 |
5.23 |
0.63 |
0.11 |
29.8 |
Inv.ex. |
[0158] In general, if the anisotropy index |Δr| obtained from the "r" values in parallel
to the sheet surface and in three directions is over 0.2, the drawability falls. Therefore,
to secure excellent formability, a |Δr| not over 2 is demanded.
[0159] The critical cooling rate was found by preparing a CCT graph. If cooling hot rolled
steel sheet by a cooling rate slower than the found critical cooling rate, the hardenability
at the time of hardening after forming a part becomes poorer and pearlite structures
are formed so sufficient strength cannot be obtained. For this reason, the critical
cooling rate must be small in order to obtain a high hardening strength. If the critical
cooling rate is 280°C/sec, it can be judged that the hardenability is improved.
[0160] In the invention examples shown in Table 3, the average carbide grain size is 0.4
to 2.0 µm, the pearlite area ratio is 6% or less, the number of grain boundary carbides/number
of grain carbides is over 1, and the I1/I0 is less than 1, so the Vickers hardness
is 100HV to 170HV in range and |Δr| is less than 0.2. In the comparative examples
using the comparative steel sheets, the Vickers hardness is over 150, while the number
of grain boundary carbides/number of grain carbides becomes less than 1. In the comparative
steel sheet in which B is not added (in Tables 1 and 2, No. 15), the critical cooling
rate is over 280°C/sec and the hardenability falls.
Example 2
[0161] A method of production of conditions outside the scope of conditions prescribed in
the present invention was applied to the 12 types of steel of the Invention Steel
Nos. 1 to 5, Nos. 16 to 19, Nos. 31, No. 33, and No. 35. Table 4 shows the manufacturing
conditions, while Table 5 shows the ferrite grain size (µm), Vickers hardness (HV),
number of grain boundary carbides/number of grain carbides, X-ray intensity ratio
I1/I0, "r" value anisotropy index |Δr|, and critical cooling rate (°C/sec) of steel
sheets produced under the manufacturing conditions shown in Table 4.
Table 4
| No |
Hot rolling conditions |
Annealing conditions |
| Finish rolling temp. (°C) |
Coiling temp. (°C) |
1st stage |
2nd stage |
Cooling rate down to 650°C (°C/hour) |
| Heating rate (°C/hour) |
Holding temp. (°C) |
Holding time (hours) |
Heating rate (°C/hour) |
Holding temp. (°C) |
Holding time (hours) |
| 1 |
720 |
520 |
60 |
710 |
24 |
60 |
740 |
5 |
80 |
| 2 |
970 |
520 |
60 |
710 |
24 |
60 |
740 |
5 |
80 |
| 3 |
920 |
350 |
60 |
710 |
24 |
60 |
740 |
5 |
80 |
| 4 |
920 |
570 |
60 |
710 |
24 |
60 |
740 |
5 |
80 |
| 5 |
920 |
520 |
60 |
600 |
24 |
60 |
740 |
5 |
80 |
| 16 |
920 |
520 |
60 |
710 |
2 |
60 |
740 |
5 |
80 |
| 17 |
920 |
520 |
60 |
710 |
24 |
60 |
720 |
5 |
80 |
| 18 |
920 |
520 |
60 |
710 |
24 |
60 |
820 |
5 |
80 |
| 19 |
920 |
520 |
60 |
710 |
24 |
60 |
740 |
18 |
80 |
| 31 |
720 |
520 |
60 |
710 |
24 |
60 |
740 |
5 |
80 |
| 33 |
920 |
520 |
60 |
600 |
24 |
60 |
740 |
5 |
80 |
| 35 |
920 |
520 |
60 |
710 |
24 |
60 |
820 |
5 |
80 |
Table 5
| No |
Ferrite grain size (µm) |
Average carbide grain size (µm) |
Pearlite area rate (%) |
Vickers hardness (HV) |
No. of grain boundary carbides/No. of grain carbides |
I1/I0 |
|Δr| |
Critical cooling rate (°C/sec) |
Remarks |
| 1 |
17 |
0.9 |
1.3 |
120 |
5.66 |
1.2 |
0.33 |
29.8 |
Comp.ex. |
| 2 |
23 |
1.1 |
2.1 |
118 |
5.85 |
1.6 |
0.47 |
29.8 |
Comp. ex. |
| 3 |
16 |
0.8 |
0.8 |
105 |
3.88 |
1.1 |
0.29 |
29.9 |
Comp.ex. |
| 4 |
13 |
1.1 |
3.1 |
109 |
5.54 |
1.3 |
0.36 |
30.0 |
Comp.ex. |
| 5 |
20 |
0.9 |
4.5 |
108 |
0.81 |
0.82 |
0.19 |
29.9 |
Comp.ex. |
| 16 |
11 |
1.1 |
3.8 |
105 |
0.53 |
0.79 |
0.18 |
30.1 |
Comp.ex. |
| 17 |
26 |
1.0 |
1.2 |
119 |
0.92 |
0.73 |
0.16 |
29.8 |
Comp.ex. |
| 18 |
13 |
2.4 |
9.4 |
161 |
0.67 |
0.68 |
0.14 |
29.6 |
Comp.ex. |
| 19 |
11 |
1.9 |
10.2 |
155 |
0.83 |
0.62 |
0.12 |
29.6 |
Comp.ex. |
| 31 |
17 |
0.9 |
0.4 |
125 |
5.72 |
1.2 |
0.33 |
29.8 |
Comp.ex. |
| 33 |
18 |
1.3 |
4.8 |
130 |
0.92 |
0.75 |
0.17 |
31.2 |
Comp.ex. |
| 35 |
18 |
1.7 |
8.2 |
163 |
0.83 |
0.75 |
0.17 |
29.5 |
Comp.ex. |
[0162] It will be understood that making the finish rolling temperature in hot rolling or
the coiling temperature a temperature outside of the scope of conditions prescribed
in the present invention invites a drop in the recrystallization and has a large effect
on the randomization of the texture and as a result causes the value of |Δr| to rise.
Further, it will be understood that if making the annealing conditions outside the
scope of conditions prescribed in the present invention, the number of grain boundary
carbides/number of grain boundary carbides becomes 1 or less and the state of distribution
of carbides greatly changes.
Industrial Applicability
[0163] As explained above, according to the present invention, it is possible to provide
steel sheet excellent in hardenability and formability as a material and a method
of production of the same. The steel sheet of the present invention is suitable for
forming a part by cold forging such as thickening to obtain a gear or other part.
Accordingly, the present invention has high applicability in the manufacture of steel
sheet and industries utilizing it.