[Technical Field]
[0001] The present invention relates to a wire rod which is raw material of PC steel stranded
wire for reinforcing a PC structure used for LNG (Liquefied Natural Gas) Tank of energy
relating facility, and which has excellent low-temperature elongation and low-temperature
toughness.
[Related Art]
[0003] LNG tank is categorized as ground type and underground type. The present invention
relates to a wire rod for ground type LNG tank and method for manufacturing the same.
As the conventional art of the ground type LNG tank, Patent document 1 proposes metal
double shell type LNG tank including a metal inner tank and a metal outer tank.
[0004] Generally, in the metal double shell type LNG tank, refrigerant is filled with clearance
between the inner tank and the outer tank to limit increases in the temperature in
the LNG tank and vaporization of LNG associated therewith. However, the structure
includes the possibility of causing damage such as outflow of a lot of LNG, if a defect
occurs at both of the inner tank and the outer tank. Therefore, in recent years, in
order to further enhance safety, a technique in which a PC dike including PC structure
(Prestressed Concrete Structure) is deployed outside the LNG tank and the inside of
the PC dike is combined with the conventional metal double shell type LNG tank appears.
[0005] The PC dike in the technique includes concrete forming circular dike enclosing the
LNG tank and PC steel stranded wire embedded in the concrete. Prestress is provided
to the PC dike by tensioning the concrete along circumferential direction using the
PC steel stranded wire. If LNG outflows from the LNG tank inside the PC dike, although
tensile stress is applied to the PC dike along the circumferential direction thereof
by the fluid pressure of the outflowing LNG, the prestress provided to the PC dike
relieves the tensile strength.
[Prior Art Document]
[Patent Document]
[Disclosure of the Invention]
[Problems to be Solved by the Invention]
[0007] On the other hand, the PC dike is continuously in a low-temperature state since heat
is drawn by the LNG in the LNG tank. In addition, if outflow of LNG occurs as described
above, LNG having temperature of -162°C or lower contacts with the concrete, and thus,
the temperature around the PC steel stranded wire reinforcing the PC dike at the inner
portion of the concrete may be greatly reduced. If low-temperature elongation and
low-temperature toughness of the PC steel stranded wire are not sufficiently high,
the PC steel stranded wire may break and the PC dike may fracture. Therefore, a wire
rod which has better low-temperature elongation and better low-temperature toughness
than the conventional wire rod for the PC steel stranded wire is needed. An object
of the present invention is to provide a wire rod which has more excellent low-temperature
elongation and more excellent low-temperature toughness than the conventional wire
rod for the PC steel stranded wire in order to meet the needs of the markets.
[Means for solving the Problem]
[0008] The inventors performed factual survey of use environment of the PC dike in order
to enhance the tension providing effect in the PC dike constructing the PC type LNG
tank (LNG tank including PC dike). As a result, in the actual use environment, it
was found that there were cases in which the wire rod was exposed to an environmental
temperature of about -40°C by heat transfer to the LNG in the LNG tank.
[0009] Therefore, various examinations with regard to a method for obtaining a wire rod
having higher low-temperature elongation and higher low-temperature toughness as compared
with the conventional PC steel stranded wire was performed. Specifically, in order
to consider about the low-temperature elongation at first, a tensile test piece having
especial shape shown in Figure 3 was manufactured from the wire rod and tensile test
was performed with the tensile test piece. In addition, in order to consider about
the low-temperature toughness, a 5mm subsize charpy impact test piece defined in JIS
Z 2202 was manufactured from the wire rod and 2mm U-notch test was performed to the
test piece to examine a relationship between the aspect of fracture surface and the
charpy absorbed energy obtained by the test. As a result of the tests, it was found
that the average grain size of pearlite block of the wire rod and a number density
of coarse pearlite block affected to the low-temperature elongation at -40°C and fracture
facet, which improve the low-temperature elongation and the low-temperature toughness.
[0010] Moreover, it was found that it was possible to provide the wire rod which had more
excellent low-temperature elongation and more excellent low-temperature toughness
as compared with the conventional wire rod for the PC steel stranded wire rod based
on the above-described findings.
[0011] That is, the gist of the present invention of which the object is to solve the above-described
problems is as follows.
[0012]
- (1) In a wire rod according to one embodiment of the present invention, a chemical
composition includes, in terms of mass%: C :0.60 to 1.20%; Si:0.30 to 1.30%; Mn:0.30
to 0.90%; P :0.020% or less; S :0.020% or less; N :0.0025 to 0.0060%; Cr:0 to 1.00%;
V :0 to 0.800%; one or more selected from the group consisting of A1:0.005 to 0.100%,
Ti:0.003 to 0.050%, and B :0.0005 to 0.0040%; and remainder including Fe and impurity,
wherein an average value of a grain size of a pearlite block in a cross section perpendicular
to a wire rod axial direction is 23 µm or less, and wherein a number density of the
pearlite blocks having 40µm or more of the grain size in the cross section perpendicular
to the wire rod axial direction is 0 to 20 pieces/mm2.
- (2) In the wire rod according to (1), the chemical composition may include one or
more selected from the group consisting of, in terms of mass%:Cr: 0.10 to 1.00%, and
V: 0.005 to 0.800%.
- (3) In the wire rod according to (1), the chemical composition may include, in terms
of mass%: C: 0.70 to 0.90%; Si: 0.80 to 1.30%; Mn: 0.60 to 0.90%; and V: 0 to 0.500%.
- (4) In the wire rod according to (3), the chemical composition may include one or
more selected from the group consisting of, in terms of mass%: Cr: 0.50 to 1.00%,
and V: 0.300 to 0.500%.
- (5) A method for manufacturing the wire rod according to the other embodiment of the
present invention, comprising: heating a steel piece having the chemical composition
according to claim 3 or 4 to a rough-rolling temperature of 950 to 1040°C and rough-rolling;
finish-wire-rolling at a finish-rolling temperature of 750 to 950°C; then, coiling
at a coiling temperature of 730 to 840°C; and thereafter, air blast cooling to a normal
temperature with a cooling rate of 15°C/sec or more, wherein the finish-rolling temperature
and a strain rate in the finish-wire-rolling satisfy an expression A,

and wherein dε / dt expresses the strain rate in the finish-wire-rolling in terms
of s-1 and T expresses the finish-rolling temperature in terms of °C.
[Advantageous Effects of Invention]
[0013] According to the above-described embodiments of the present invention, a wire rod
for PC steel stranded wire which is favorable to usage as tendon of PC dike of PC-type
LNG tank and which has more excellent elongation and toughness at about -40°C as compared
with the conventional material can be provided by reducing the grain size of pearlite
block and limiting the number density of coarse pearlite block.
[Brief Description of Drawings]
[0014]
Figure 1 is a graph indicating a relationship between an average grain size of pearlite
block of the wire rod and reduction of area of the wire rod.
Figure 2 is a graph indicating a relationship between Z value in manufacturing the
wire rod and the grain size of the pearlite block of the wire rod.
Figure 3 indicates a shape of low temperature tensile test piece.
Figure 4 indicates a collection position of 5mm subsize charpy impact test piece defined
in JIS Z 2202.
Figure 5A indicates a grain size of the pearlite block of the example manufactured
with a stelmor method.
Figure 5B indicates the grain size of the pearlite block of the comparative example.
Figure 6 indicates elongation of an example (No. 6) and a comparative example (No.
17) at -40°C.
Figure 7A indicates a grain size of the pearlite block of the example manufactured
with DLP method.
Figure 7B indicates a grain size of the pearlite block of the comparative example.
Figure 8 indicates a relationship between pearlite block size (µm) and an absorbed
energy (Charpy impact value) (J).
Figure 9A is a photograph indicating an observation result of a fracture surface of
the impact test piece of the example with SEM.
Figure 9B is a photograph indicating an observation result of a fracture surface of
the impact test piece of the comparative example with SEM.
Figure 10 is a flow chart indicating an example of a method for manufacturing the
wire rod with a stelmor method.
[Description of Embodiments]
[0015] In a wire rod for PC steel stranded wire according to the present embodiment (hereinafter
"a wire rod according to the present embodiment") having excellent low-temperature
elongation and low-temperature toughness, a chemical composition includes, in terms
of mass%: C :0.60 to 1.20%; Si:0.30 to 1.30%; Mn:0.30 to 0.90%; P :0.020% or less;
S :0.020% or less; N :0.0025 to 0.0060%; Cr:0 to 1.00%; V :0 to 0.800%; one or more
selected from the group consisting of A1:0.005 to 0.100%, Ti:0.003 to 0.050%, and
B :0.0005 to 0.0040%; and remainder including Fe and impurity, wherein an average
value of a grain size of a pearlite block is 23µm or less in a cross section perpendicular
to a wire rod axial direction, and wherein the number density of the pearlite block
having 40µm or more of the grain size is 0 to 20 pieces/mm
2 in the cross section perpendicular to the wire rod axial direction.
[0016] At first, a reason for limiting the chemical composition of the wire rod according
to the present embodiment will be described. Hereinafter, "%" expresses "mass%".
(C: 0.60 to 1.20%)
[0017] C is an element having an effect of increasing a cementite ratio in the wire rod
to increase strength of the wire rod. A lamellar spacing of the pearlite can be controlled
by adjusting a patenting condition, and the strength of the wire rod can be increased
by working. On the other hand, if an amount of C is less than 0.60%, a strength which
can sufficiently tension a PC dike of a PC-type LNG tank cannot be obtained even if
the above-described adjusting the patenting condition is performed.
[0018] If the amount of C in the wire rod is more than 1.20%, a mesh-shaped cementite forms
in a structure in the wire rod. The mesh-shaped cementite may frequently cause breaking
during wire drawing and may interfere production activity of the wire rod.
[0019] As a method for manufacturing the wire rod according to the present embodiment, both
of DLP (Direct in-Line Patenting) method and stelmor method can be employed as follows.
If the wire rod is manufactured with the stelmor method, it is preferable that the
amount of C be 0.70 to 0.90%. If the wire rod is manufactured with the stelmor method,
a cooling rate of the wire rod is lower than that in the manufacturing with the DLP
method, and thus, the elongation and the toughness of the wire rod is relatively low.
In order to compensate for the decrease in the strength, it is preferable that the
lower limit of the amount of C be 0.70%. In addition, if the amount of C excessively
increases, a pro-eutectoid cementite forms in the mesh shape at a grain boundary of
prior austenite during cooling the wire rod, since the wire rod becomes a hyper-eutectoid
steel (a steel having a structure containing both of pearlite and cementite). The
mesh-shaped pro-eutectoid cementite significantly deteriorates the drawability of
the wire rod. In order to prevent the mesh-shaped pro - eutectoid cementite from forming,
it is preferable that the upper limit of the amount of C be 0.90%. It is more preferable
that the amount of C be 0.80 to 0.90%.
(Si: 0.30 to 1.30%)
[0020] Si is an element which acts as a deoxidizing element during refining. When 0.30%
or more of Si is included, the deoxidizing effect is sufficiently expressed. Therefore,
the lower limit of the amount of Si of the wire rod according to the present embodiment
is 0.30%. Si also includes an effect for enhancing the strength of the wire rod. When
0.80% or more of Si is included, the effect of enhancing the strength is expressed.
Therefore, the lower limit of the amount of Si of the wire rod according to the present
embodiment may be 0.80%. In addition, although Si solid-solute strengthen ferrite,
Si has an effect for rising a nose of isothermal transformation during heat treatment.
Therefore, an excessive amount of Si increases cost for the heat treatment. Accordingly,
in view of a capacity of the manufacturing equipments, the upper limit of the amount
of Si is 1.30%.
[0021] As the method for manufacturing the wire rod according to the present embodiment,
both of the DLP method and the stelmor method can be employed. If the wire rod is
manufactured with the stelmor method, it is preferable that the amount of Si be 0.80
to 1.30%. If the wire rod is manufactured with the stelmor method, a cooling rate
of the wire rod is lower than that in the manufacturing with the DLP method, and thus,
the elongation and the toughness of the wire rod is relatively low. In order to compensate
the decreasing of the strength, it is preferable that the lower limit of the amount
of Si be 0.80%. It is more preferable that the amount of Si be 0.90 to 1.25%.
(Mn: 0.30 to 0.90%)
[0022] Mn is an solid-solute strengthening element and has an effect of enhancing elongation
and toughness of the wire rod and an effect of enhancing hardenability. In order to
secure elongation and toughness of the wire rod, it is necessary that 0.30% or more
of Mn be included. In addition, in order to further enhance the elongation of the
wire rod, the lower limit of the amount of Mn may be 0.60%. On the other hand, if
the amount of Mn is higher than 0.90%, a delay of transformation occurs in a center
portion of the wire rod to cause a formation of micro martensite at a portion of untransformed
austenite during manufacturing the wire rod. The micro martensite at the center portion
of the wire rod causes breaking during drawing of the wire rod. Therefore, it is necessary
that the upper limit of the amount of Mn is 0.90%.
[0023] As the method for manufacturing the wire rod according to the present embodiment,
both of the DLP method and the stelmor method can be employed. If the wire rod is
manufactured with the stelmor method, it is preferable that the amount of Mn be 0.60
to 0.90%. If the wire rod is manufactured with the stelmor method, the cooling rate
of the wire rod is lower than that in the manufacturing with the DLP method, and thus,
the elongation and the toughness of the wire rod is relatively low. In order to compensate
the decreasing of the strength, it is preferable that the lower limit of the amount
of Mn be 0.60%. It is more preferable that the amount of Mn be 0.70 to 0.90%.
(P: 0.020% or lower)
(S: 0.020% or lower)
[0024] P has an effect of embrittling the steel. Therefore, it is necessary that an upper
limit an amount of P is 0.020%. When the wire rod is further securely prevented from
low-temperature embrittlement, the upper limit of the amount of P may be 0.010%, 0.005%,
or 0.001%.
[0025] S is an element which combines with Mn in the wire rod to form MnS. Since S segregates
at a center portion of the steel during refining and solidifying the steel, MnS accumulates
at the center portion of the steel. MnS deteriorates the low-temperature elongation
of the steel. If an amount of S is more than 0.020%, the low-temperature elongation
significantly deteriorates, and thus, the amount of S is 0.020% or lower. When the
wire rod is further securely prevented from the low-temperature embrittlement, the
upper limit of the amount of S may be 0.010%, 0.005%, or 0.001%.
[0026] In the wire rod according to the present embodiment, the lower the amount of P and
the amount of S are, the better it is. Therefore, both of the lower limit of the amount
of P and the lower limit of the amount of S is 0%.
(N: 0.0025 to 0.0060%)
[0027] N is an element which combines with Al, Ti, and B to form nitrides. The nitrides
act as a nucleuses of precipitation of the austenite, and thus, the grain size of
the austenite can be controlled during heating the steel by controlling the number
of the nitrides. If the amount of the nitrides increase, the grain is refined. If
the amount of N is less than 0.0025%, the nitrides do not sufficiently form and the
effect of refining the grain size cannot be sufficiently obtained. On the other hand,
If the amount of N is more than 0.0060%, free N, which does not combine with Al, Ti,
and B, become excess. The excess amount of free N causes age hardening to deteriorate
the elongation and the toughness of the wire rod. Therefore, it is necessary that
the amount of N be 0.0025 to 0.0060%. It is preferable that the amount of N be 0.0025
to 0.0040%.
[0028] In addition to the above-described elements, the wire rod according to the present
embodiment further includes one or more selected from the group consisting of Al:
0.005 to 0.100%, Ti: 0.003 to 0.050%, and B: 0.0005 to 0.0040%.
(Al: 0.005 to 0.100%)
[0029] Al acts as a deoxidizing agent during refining the steel. In addition, since Al forms
composition with N in the steel, Al has an effect of fixing N. Due to fixing N, the
steel can be prevented from age hardening. Furthermore, when B is included together
with Al, due to fixing N, the amount of solute B can be increased.
[0030] However, if an amount of Al is less than 0.005%, the effect of fixing N by Al cannot
be sufficiently obtained. On the other hand, if the amount of A1 is more than 0.100%,
Al
2O
3, which is formed by Al combining with oxygen in the steel, forms clusters. The clusters
act as origins of cracking during drawing. Therefore, the amount of Al may be 0.005
to 0.100%. It is preferable that the amount of Al be 0.020 to 0.050%.
(Ti: 0.003 to 0.050%)
[0031] Ti acts as the deoxidizing agent of the steel, similar to Al. In addition, since
Ti forms chemical compound with N in the steel, Ti has an effect of fixing N. Due
to fixing N, the steel can be prevented from age hardening. Furthermore, when B is
included together with Ti, due to fixing N, the amount of solute B can be increased.
[0032] However, if the amount of Ti is less than 0.003%, the effect of fixing N by Ti cannot
be sufficiently obtained. On the other hand, if the amount of Ti is more than 0.050%,
TiC, which is formed by Ti combining with carbon in the steel, increase. TiC act as
an origins of cracking during drawing. Therefore, the amount of Ti may be 0.003 to
0.050%. It is preferable that the amount of Ti be 0.020 to 0.040%.
[0033] As described above, Al and Ti have similar effects. Therefore, the amount of Al can
be decreased by including Ti. In this case, a similar effect can be obtained.
(B: 0.0005 to 0.0040%)
[0034] When B exists as the solute B in the austenite, B has an effect of enhancing the
hardenability of the wire rod. If the amount of B is less than 0.0005%, the effect
of enhancing the hardenability cannot be sufficiently obtained. On the other hand,
if the amount of B is more than 0.0040%, B forms chemical compound with Fe and C to
form a precipitates such as Fe
23 (C, B)
6, and the like. The precipitates act as the origins of cracking during drawing. Therefore,
the amount of B may be 0.0005 to 0.0040%. It is preferable that the amount of B be
0.0009% to 0.0030%.
[0035] In addition to the above-described elements, the wire rod according to the present
embodiment may further include, in terms of mass%, Cr: 0 to 1.00% or V: 0 to 0.800%.
(Cr: 0 to 1.00%)
[0036] In the wire rod according to the present embodiment, it is not necessary to include
Cr. Therefore, a lower limit of an amount of Cr is 0%. However, Cr has an effect of
reducing lamellar spacing of the pearlite to enhance the strength of the wire rod.
Due to the effect, the degree of increasing of the strength of the wire rod during
drawing is enhanced. The effect is obtained in a case in which the amount of Cr is
0.10% or more, and thus, it is preferable that the amount of Cr be 0.10% or more.
In addition, when the strength is further enhanced, it is preferable that 0.50% or
more of Cr be included. If the amount of Cr is more than 1.00%, a termination time
of pearlite transformation becomes long, and thus, a supercooled structure forms during
cooling the wire rod to deteriorate the elongation of the wire rod. Therefore, it
is preferable that an upper limit of the amount of Cr be 1.00%.
[0037] As the method for manufacturing the wire rod according to the present embodiment,
both of the DLP method and the stelmor method can be employed. If the wire rod is
manufactured with the stelmor method, it is more preferable that the amount of Cr
be 0.50 to 1.00%. If the wire rod is manufactured with the stelmor method, the cooling
rate of the wire rod is lower than that in the manufacturing with the DLP method,
and thus, the elongation and the toughness of the wire rod is relatively low. In order
to compensate the decreasing of the strength, it is more preferable that the lower
limit of the amount of Cr be 0.50%. It is further preferable that the amount of Cr
be 0.50 to 0.90%.
(V: 0 to 0.800%)
[0038] In the wire rod according to the present embodiment, it is not necessary to include
V. Therefore, a lower limit of an amount of V is 0%. However, V is an element which
combines with C to precipitate as carbide in ferrite. Due to the precipitation of
the carbide, the ferrite can be hardened and the wire rod can be high-strengthened.
The effect can be obtained if 0.005% or more of V is included. However, if the amount
of V is more than 0.800%, a coarse carbides precipitate. The coarse carbides act as
the origins of cracking in working the wire rod. Therefore, it is preferable that
the amount of V be 0.005 to 0.800%.
[0039] As the method for manufacturing the wire rod according to the present embodiment,
both of the DLP method and the stelmor method can be employed. If the wire rod is
manufactured with the stelmor method, it is more preferable that the amount of V be
0.300 to 0.500%. If the wire rod is manufactured with the stelmor method, the cooling
rate of the wire rod is lower than that in the manufacturing with the DLP method,
and thus, the elongation and the toughness of the wire rod is relatively low. In order
to compensate the decreasing of the strength, it is more preferable that the lower
limit of the amount of V be 0.300%. In addition, since micro cracks form at boundary
portions of VC precipitates and base iron when a processing strain occurs, it is more
preferable that an upper limit of the amount of V be 0.500%. It is further preferable
that the amount of V be 0.300 to 0.400%.
(remainder: Fe and impurity)
[0040] Remainder of the wire rod according to the present embodiment includes Fe and impurity.
The impurity is a component which is incorporated by raw materials such as mineral
or scrap or various factors of a manufacturing process when the steel is industrially
manufactured, and is accepted within a range that does not adversely affect the property
of the wire rod according to the present embodiment.
(The average value of the grain size of a pearlite block in a cross section perpendicular
to a wire rod axial direction: 23µm or less.)
[0041] In the present embodiment, a pearlite block boundary is defined as a boundary of
adjacent two pearlites between which a difference in crystal orientation is 9° or
higher, a pearlite block is defined as an area surrounded by the pearlite block boundary,
and PBS (Pearlite Block Size) is defined as an equivalent circle diameter of the pearlite
block. In the wire rod according to the present embodiment, in addition to the above-described
definition of the chemical composition, an average PBS (Pearlite Block Size) in a
cross section perpendicular to a wire rod axial direction is defined to 23µm or less.
[0042] If the average PBS (Pearlite Block Size) is more than 23µm, a reduction of area of
the wire rod deteriorates. It is necessary that the wire rod according to the present
embodiment has 30% or more of the reduction of area. In view of the past production
result, it was found that 30% or more of the reduction of area was necessary to prevent
breaking from causing during drawing in the drawing working of the wire rod. As a
result of the inventor's consideration, it was found that there was a relationship
indicated by a graph of Figure 1 between the average pearlite block size and the reduction
of area. Figure 1 indicates that 30% or more of the reduction of area can be obtained
when the average PBS (Pearlite Block Size) is 23µm or less. In addition, when the
average PBS (Pearlite Block Size) is more than 23µm, frequency of branching of the
crack end decreases. Since a branch of the crack end has an effect of suppressing
crack propagation, decreasing the frequency of branching of the crack end enlarges
a fracture facet to deteriorate the low-temperature elongation and the low-temperature
toughness. Therefore, the average PBS (Pearlite Block Size) is 23µm or less. It is
preferable that the average pearlite block size be 18µm or less.
[0043] The average value of the equivalent circle diameter of the pearlite block in any
size of field of view at any position of the cross section perpendicular to the wire
rod axial direction can be obtained by using EBSD device. The average PBS in the cross
section perpendicular to the wire rod axial direction according to the present embodiment
can be obtained by the following procedures. At first, average values (primary average
values) of equivalent circle diameters of pearlite blocks in 300µm × 180µm of fields
of view in each of five area consisting of
- (1) a surface part (an area of which a depth from a surface of the wire rod is 30µm),
- (2) a 1/4D part (an area of which a depth from the surface of the wire rod is 1/4
of a diameter D of the wire rod),
- (3) a center part,
- (4) a 3/4D part (an area of which a depth from the surface of the wire rod is 3/4
of a diameter D of the wire rod, i.e. an area opposite to the (2) with respect to
the center part of the wire rod), and
- (5) an opposite surface part (i.e. an area opposite to the (1) with respect to the
center part of the wire rod),
are measured by using the EBSD device. Then, the average value (secondary average
value) of the each primary average values is calculated. The secondary average value
is the average PBS in the cross section perpendicular to the wire rod axial direction
according to the present embodiment.
(The number density of the pearlite block having 40µm or more of grain size in the
cross section perpendicular to the wire rod axial direction is 0 to 20 pieces/mm2.)
[0044] In the wire rod according to the present embodiment, in addition to the above-described
definition of the chemical composition and the average value of the grain size of
the pearlite block, the number density of the pearlite block having a grain size of
40µm or more in the cross section perpendicular to the wire rod axial direction is
defined to 0 to 20 pieces/mm
2.
[0045] Since the pearlite blocks having 40µm or more of grain size act as fracture origins,
the pearlite blocks having 40µm or more of grain size deteriorate the elongation and
the toughness of the wire rod even if the number of the pearlite blocks having 40µm
or more of grain size is small. In addition to controlling the average value of the
grain size of the pearlite block, in the wire rod according to the present embodiment,
it is necessary that a coarse pearlite block is prevented from forming. For these
reasons, the number density of the coarse pearlite blocks is limited. Hereinafter,
"pearlite block having a grain size of 40µm or more" may be referred to as "coarse
pearlite block" or "coarse PB".
[0046] If the number density of the coarse pearlite blocks in the cross section perpendicular
to the wire rod axial direction is more than 20 pieces/mm
2, the elongation and the toughness of the wire rod do not satisfy required levels.
Therefore, it is necessary that the number density of the coarse pearlite blocks in
the cross section perpendicular to the wire rod axial direction is limited to 0 to
20 pieces/mm
2. It is preferable that an upper limit of the number density of the coarse pearlite
blocks in the cross section perpendicular to the wire rod axial direction be 18 pieces/mm
2. The less the amount of the coarse pearlite blocks are, the more preferable it is,
and therefore, the lower limit of the number density of the coarse pearlite blocks
in the cross section perpendicular to the wire rod axial direction is 0 pieces/mm
2.
[0047] The number density of the pearlite blocks having a grain size of 40µm or more in
any size of field of view at any position of the cross section perpendicular to the
wire rod axial direction can be obtained by using EBSD device. The number density
of the pearlite blocks having 40µm or more of grain size in the cross section perpendicular
to the wire rod axial direction according to the present embodiment can be obtained
by the following procedures. At first, the number densities of the pearlite blocks
having a grain size of 40µm or more in 300µm × 180µm of fields of view in each of
five areas of
- (1) a surface part (an area of which a depth from a surface of the wire rod is 30µm),
- (2) a 1/4D part (an area of which a depth from the surface of the wire rod is 1/4
of a diameter D of the wire rod),
- (3) a center part,
- (4) a 3/4D part (an area of which a depth from the surface of the wire rod is 3/4
of a diameter D of the wire rod, i.e. an area opposite to the (2) with respect to
the center part of the wire rod), and
- (5) an opposite surface part (i.e. an area opposite to the (1) with respect to the
center part of the wire rod),
are measured by using the EBSD device. Then, the average value of the number densities
in each areas is calculated. The average value is the number density of the pearlite
block having a grain size of 40µm or more in the cross section perpendicular to the
wire rod axial direction according to the present embodiment.
[0048] Then, a method for manufacturing the wire rod according to the present embodiment
will be described.
[0049] There are DLP method and stelmor method as the method for manufacturing the wire
rod according to the present embodiment.
[0050] When the wire rod according to the present embodiment is manufactured by the stelmor
method, as shown in Figure 10, (1) heating a steel piece having a chemical composition
including, in terms of mass%, C: 0.70 to 0.90%; Si: 0.80 to 1.30%; Mn: 0.60 to 0.90%;
P: 0.020% or less; S: 0.020% or less; N: 0.0025 to 0.0060%; Cr: 0 to 1.00%; V: 0 to
0.500%; one or more selected from the group consisting of Al: 0.005 to 0.100%, Ti:
0.003 to 0.050%, and B: 0.0005 to 0.0040%; and remainder including Fe and impurity
to a rough-rolling temperature of 950 to 1040°C and then rough-rolling, (2) finish-wire-rolling
at a finish-rolling temperature of 750 to 950°C, (3) coiling at a coiling temperature
of 730 to 840°C, and (4) air blast cooling to a normal temperature with a cooling
rate of 15°C/sec or more are performed. In this case, it is necessary that the finish-rolling
temperature and a strain rate satisfy a relation of following expression 1.

[0051] dε / dt expresses the strain rate during the finish-wire-rolling in terms of s
-1 and T expresses the finish-rolling temperature in terms of °C.
[0052] When manufacturing with stelmor method is performed, the steel piece may further
include, in terms of mass%, one or more selected from the group consisting of Cr:
0.50 to 1.00%, and V: 0.300 to 0.500%.
(The chemical composition of a steel piece used for rough-rolling: within defined
range as described above.)
[0053] When the wire rod according to the present embodiment is manufactured by the stelmor
method, it is necessary that the chemical composition of a steel piece used for rough-rolling
is within defined range as described above. The defined range is narrower than the
above-described defined range of the chemical composition of the wire rod according
to the present embodiment. The stelmor method is a manufacturing method in which air
blast cooling is performed after coiling, and the cooling rate by the air blast cooling
is lower than a cooling rate of a direct heat treatment by a molten salt in a DLP
method described below. When the cooling rate is low, the elongation and the toughness
of the wire rod finally obtained are relatively low.
[0054] Therefore, in a case in which the wire rod according to the present embodiment is
manufactured by the stelmor method, it is necessary that the amount of C, Mn, and
Si which are alloy elements for enhancing the elongation and the toughness are more
than that in a case of performing the direct heat treatment by the molten salt in
the DLP method. In addition, in a case in which Ca and V are included in order to
enhance the property of the wire rod when the wire rod according to the present embodiment
is manufactured with stelmor method, it is preferable that the amount of Cr and V
be also more than that in the case of performing the direct heat treatment by the
molten salt in the DLP method.
(heating temperature of the steel piece before rough-rolling)
[0055] In the method for manufacturing the wire rod according to the present embodiment
with stelmor method, a heating temperature of the steel piece before the rough-rolling
(rough-rolling temperature) is 950 to 1040°C. If the heating temperature of the steel
piece before rough-rolling is lower than 950°C, roll reaction forth in wire rod rolling
may rapidly increase to cause trouble of the equipment such as cracking of roll. Therefore,
the heating temperature of the steel piece before the rough-rolling is 950°C or more.
On the other hand, if the heating temperature of the steel piece before the rough-rolling
is more than 1040°C, solutionizing of aluminum nitride (AlN) precipitated in the steel
piece progresses excessively. As described above, AlN act as the nucleuses of precipitation
of the austenite to contribute to refine the grain size of the austenite. The grain
size of the pearlite of the wire rod finally obtained can be refined by refining the
grain size of the austenite of the wire rod during manufacturing stage. However, if
the solutionizing of AlN progresses excessively, coarsening the grain size of the
austenite progresses. In this case, PBS of the wire rod is coarsened after manufacturing
the wire rod. In this case, the average value of the grain size of the pearlite block
in the cross section perpendicular to the wire rod axial direction becomes more than
23µm, and/or the number density of the pearlite block having 40µm or more of the grain
size becomes more than 20 pieces/mm
2. In order to avoid such phenomenon from causing, the heating temperature of the steel
piece before the rough-rolling is 1040°C or lower.
(a temperature in finish-wire-rolling: 750 to 950°C)
[0056] In the method for manufacturing the wire rod according to the present embodiment
with stelmor method, finish-wire-rolling is performed at a temperature range of 750
to 950°C. If the temperature in the finish-wire-rolling (finish-rolling temperature)
is less than 750°C, roll reaction forth during rolling may increase to cause trouble
of the equipment such as cracking of roll, and thus, the temperature in the finish-wire-rolling
is 750°C or more. On the other hand, if the temperature during the finish-wire-rolling
is more than 900°C, the grain size of the austenite coarsens. In this case, the average
value of the grain size of the pearlite block in the cross section perpendicular to
the wire rod axial direction becomes more than 23µm, and/or the number density of
the pearlite blocks having 40µm or more of the grain size becomes more than 20 pieces/mm
2. The elongation of the wire rod is deteriorated by coarsening the pearlite block.
In order to avoid such phenomenon, the temperature during the finish-wire-rolling
is 900°C or lower.
[0057] (relation between the finish-rolling temperature and a strain rate in the finish-wire-rolling:
13.7 ≤ log
10 Z ≤ 16.5)
[0058] In addition, in the method for manufacturing the wire rod according to the present
embodiment with stelmor method, it is necessary that a relation between the finish-rolling
temperature and a strain rate in the finish-wire-rolling is defined. Specifically,
it is necessary that common logarithm (log
10 Z) of Z value (Zener-Hollomon parameter) is 13.7 to 16.5, in which the Z value is
obtained by substituting a strain rate of the wire rod at the finish-wire-rolling
dε / dt, an activation energy of plastic deformation of the wire rod Q, and the finish-rolling
temperature at the finish-wire-rolling T into the following expression 2 which indicates
Zener-Hollomon expression.

[0059] "dε / dt" expresses the strain rate in terms of s
-1. "R" is gas constant and the value thereof is 1.98 cal/mol·deg. "T" expresses the
finish-rolling temperature in terms of K. If the term of the finish-rolling temperature
is °C, it is necessary that "T" in the expression 2 is replaced by "(T + 273.15)".
"Q" expresses the activation energy of the plastic deformation of the wire rod. It
is assumed that the activation energy of the plastic deformation of the wire rod according
to the present embodiment having the above-described chemical composition is 63800
cal/mol.
[0061] "ε" is an amount of strain during the finish-wire-rolling and is a dimensionless
parameter. "h1" is a diameter of the wire rod before the finish-wire-rolling in terms
of mm, and "h2" is a diameter of the wire rod after the finish-wire-rolling in terms
of mm. "N" is a number of revolution of a roll performing the finish-wire-rolling
in terms of rpm. "L
d" is a projected roll contact length during the finish-wire-rolling in terms of mm.
The projected roll contact length is the length of an area, at which the roll contacts
with a rolled material (wire rod) during the rolling, along the rolling direction.
"r" is a radius of the roll at the finish-wire-rolling in terms of mm. "Δh" is a rolling
reduction during the finish-wire-rolling in terms of mm. As shown in expressions 3
to 6, the strain rate is a rolling condition depending on both of rolling speed and
rolling reduction.
[0062] As a result of the inventor's consideration, it was found that there was a relationship
indicated in Figure 2 between the Z value at the finish-wire-rolling and the average
pearlite block size of the wire rod finally obtained. As shown in Figure 2, in order
to control the average pearlite block size in the cross section perpendicular to the
wire rod axial direction to 23µm or less, it is necessary that log
10 Z be 13.7 or more. In addition, in order to control the number density of the coarse
pearlite blocks having 40µm or more of grain size to 0 to 20 pieces/mm
2, as is the case with that, it is necessary that log
10 Z is 13.7 or more. On the other hand, in view of the equipment capacity, it is difficult
to set log
10 Z to more than 16.5. As shown in the Zener-Hollomon expression, in order to increase
Z value, it is necessary to decrease the rolling temperature and increase the strain
rate. Therefore, in the method for manufacturing the wire rod according to the present
embodiment with stelmor method, the upper limit of log
10 Z is 16.5. It is preferable that log
10 Z be 14.0 to 16.0. If log
10 Z is lower than above-described range, the average value of the grain size of the
pearlite block in the cross section perpendicular to the wire rod axial direction
becomes more than 23µm, and/or the number density of the pearlite block having 40µm
or more of the grain size becomes more than 20 pieces/mm
2.
[0063] The speed of the finish-wire-rolling (finish rolling speed) is not limited as long
as log
10 Z is within the range of 13.7 to 16.5. It is preferable that, if a wire rod having
a diameter of 12mm or more is manufactured, the speed of the finish-wire-rolling be
15.5 to 25.2 m/sec. If the speed of the finish-wire-rolling is less than 15.5 m/sec,
the strain rate decreases. In this case, PBS may not be sufficiently reduced. Therefore,
it is preferable that the speed of the finish-wire-rolling be 15.5 m/sec or more.
On the other hand, if the speed of the finish-wire-rolling is more than 25.2 m/sec,
exotherm during working may increase to coarsen the grain size of austenite. Also
in this case, PBS cannot be refined. As shown in above-described expressions 3 to
6, when a wire rod of which the diameter is not 12 mm, it is necessary that the speed
of the finish-wire-rolling is arbitrarily changed from the above-described range so
that log
10 Z is within the range of 13.7 to 16.5.
(coiling temperature: 730 to 840°C)
(air blast cooling rate after coiling: 15°C/sec or more)
[0064] In the method for manufacturing the wire rod according to the present embodiment
with stelmor method, after the finish-wire-rolling, the wire rod is coiled at a temperature
of 730 to 840°C, and then, air blast cooling is performed with a cooling rate of 15°C/sec
or more. If the coiling temperature is lower than 730°C, the amount of scale decreases
to deteriorate mechanical descalability, and thus, the coiling temperature is 730°C
or more. If the coiling temperature is higher than 840°C, the grain size of the austenite
increases. In this case, the grain size of the pearlite block of the wire rod finally
obtained cannot be controlled to 23µm or less, and/or the number density of the pearlite
blocks having 40µm or more of the grain size becomes more than 20 pieces/mm
2. Therefore, the coiling temperature is 840°C or lower. It is preferable that the
coiling temperature be 750 to 820°C.
[0065] The wire rod after the coiling is cooled by air blast cooling to a normal temperature.
The normal temperature basically indicates a temperature range of 5 to 35°C as defined
in JIS Z 8703. In the case, if the cooling rate is lower than 15°C/sec (i.e. slow
cooling), the grain size of austenite increases, and thus, the average value of the
grain size of the pearlite block in the cross section perpendicular to the wire rod
axial direction becomes more than 23µm, and/or the number density of the pearlite
block having 40µm or more of the grain size becomes more than 20 pieces/mm
2. As a result, the elongation of the wire rod finally obtained deteriorates. Therefore,
the cooling rate at the air blast cooling is 15°C/sec or more. It is preferable that
the cooling rate at the air blast cooling be 25°C/sec or more. Although it is not
necessary to define the upper limit of the cooling rate at the air blast cooling,
in view of the equipment capacity, the upper limit is about 50°C/sec.
[0066] When the wire rod according to the present embodiment is manufactured by the DLP
method, (1) heating a steel piece having a chemical composition including, in terms
of mass%, C: 0.60 to 1.20%; Si: 0.30 to 1.30%; Mn: 0.30 to 0.90%; P: 0.020% or less;
S: 0.020% or less; N: 0.0025 to 0.0060%; Cr: 0 to 1.00%; V: 0 to 0.500%; one or more
selected from the group consisting of Al: 0.005 to 0.100%, Ti: 0.003 to 0.050%, and
B: 0.0005 to 0.0040%; and remainder including Fe and impurity to a temperature of
950 to 1040°C and wire rod rolling, (2) coiling at a temperature range of 750 to 800°C,
and (3) direct heat treating with 500 to 600°C of a molten salt just after termination
of the coiling are performed.
[0067] When the wire rod according to the present embodiment is manufactured with DLP method,
the steel piece, which is raw material, may further include, in terms of mass%, one
or more selected from the group consisting of Cr: 0.10 to 1.00%, and V: 0.005 to 0.800%.
(a chemical composition of a steel piece used for wire rod rolling: within defined
range as described above)
[0068] When the wire rod according to the present embodiment is manufactured by the DLP
method, it is necessary that a chemical composition of a steel piece used for wire
rod rolling is within defined range as described above. The defined range is equal
to the above-described defined range of the chemical composition of the wire rod according
to the present embodiment. A method for manufacturing with DLP method has an advantage
that a wire rod having excellent elongation and toughness can be obtained from a steel
piece of which alloy elements for enhancing the elongation and the toughness is relatively
low. However, direct heat treatment with molten salt is essential the for the method
for manufacturing with the DLP method, and thus, in order to bring the method for
manufacturing with the DLP method into operation, much more equipment is required
than that with the stelmor method.
(heating temperature in wire rod rolling: 950 to 1040°C)
[0069] When the wire rod according to the present embodiment is manufactured by the DLP
method, the heating temperature of the wire rod before wire rod rolling the steel
piece is 950 to 1040°C. If the heating temperature is lower than 950°C, roll reaction
forth during the wire rod rolling may considerably increase to cause troubles in equipments
such as cracking of roll, and thus, the heating temperature before the wire rod rolling
is 950°C or more. On the other hand, if the heating temperature before the wire rod
rolling is higher than 1040°C, solutionizing of aluminum nitride (AlN) precipitated
in the steel piece progresses, and thus, coarsening the grain size of the austenite
progresses to coarsen the pearlite block size (PBS) of the wire rod finally obtained.
In this case, the average value of the grain size of the pearlite block in the cross
section perpendicular to the wire rod axial direction becomes more than 23µm, and/or
the number density of the pearlite blocks having 40µm or more of the grain size becomes
more than 20 pieces/mm
2. In order to avoid such phenomenon from causing, the heating temperature before the
wire rod rolling is 1040°C or lower. It is preferable that the heating temperature
before the wire rod rolling be 980 to 1030°C. The finish temperature at the wire rod
rolling is not limited, and thus, a reasonable temperature can be arbitrarily selected.
(coiling temperature: 750 to 850°C)
[0070] When the wire rod according to the present embodiment is manufactured by the DLP
method, coiling temperature after the wire rod rolling is 750 to 850°C. If the coiling
temperature is lower than 750°C, unevenness along longitudinal direction of the wire
rod regarding tensile strength increases after isothermal transformation in the following
isothermal transformation treating. Therefore, the coiling temperature is 750°C or
higher. If the coiling temperature is higher than 800°C, the grain size of austenite
increases. In this case, the grain size of the pearlite block of the wire rod finally
obtained cannot be controlled to 23µm or less and the number density of the pearlite
block having 40µm or more of the grain size cannot be controlled to be 20 pieces/mm
2 or less, and thus, the coiling temperature is 800°C or lower.
(method for isothermal transformation treating: direct heat treating)
(isothermal transformation treating temperature: 500 to 600°C)
[0071] When the wire rod according to the present embodiment is manufactured by the DLP
method, immediately after coiling the wire rod, the wire rod is immersed into 500
to 600°C of molten salt to perform isothermal transformation treating. If the isothermal
transformation treating temperature is lower than 500°C, many amount of non-pearlite
structure forms at the surface part of the wire rod. In this case, unevenness of processing
strain occurs at boundary between pearlite structure forming at internal part of the
wire rod and the non-pearlite structure at the surface part, and the unevenness may
cause breaking during wire drawing stage. Therefore, the isothermal transformation
treating temperature is 500°C or higher. If the isothermal transformation treating
temperature is higher than 600°C, operational problems such as increasing heat deformation
of the equipment occurs, and thus, the isothermal transformation treating temperature
is 600°C or lower. In addition, it is necessary that the isothermal transformation
treatment is performed with direct heat treatment (online heat treatment). If the
direct heat treatment is not performed (i.e. the isothermal transformation treatment
is performed with offline heat treatment), reheating included in the offline heat
treatment causes growth of y grain. The phenomenon prevents the grain size of PBS
of the wire rod from being controlled to 23µm or less.
[Examples]
[0072] Hereinafter, examples of the present invention will be described. The conditions
in manufacturing the examples are an example condition employed to confirm the operability
and the effects of the present invention, so the present invention is not limited
to the example condition. The present invention can employ various types of conditions
as long as the conditions do not depart from the scope of the present invention and
can achieve the object of the present invention.
(Example)
[0073] Hereinafter, examples by a method for manufacturing with stelmor method will be described.
[0074] At first, molten steel having chemical composition shown in Table 1-1 was continuously
casted so as to be a cast bloom of 300mm × 500mm, and the cast bloom is rolled so
as to be a steel billet of 122mm square by blooming. Then, the steel billet was heated
to a heating temperature shown in Table 1-2 and rolled under a condition shown in
the Table 1-2 to obtain a wire rod of 12mmϕ. A radius of a roll in finish-wire-rolling
was 75.5mm. No. S1 to S16 are examples which satisfy the condition according to the
present invention and No. S 17 to S41 are comparative examples which do not satisfy
the condition according to the present invention.
[0075] A tensile test pieces shown in Figure 3 were manufactured from the rolled wire rods.
Tensile test was performed to the tensile test pieces at a low temperature atmosphere
of -40°C while controlling the temperature using dry ice and alcohol to measure tensile
strength and elongation at -40°C of the wire rod.
[0076] In addition, a charpy impact test pieces defined in JIS Z 2202 were extracted from
the above-described wire rods in a manner of extracting shown in Figure 4 to manufacture
5mm subsize 2mm U-notch charpy impact test pieces. Charpy impact test at -40°C was
performed to the charpy impact test pieces to obtain impact value of the wire rods
at a temperature of -40°C, which was similar to actual using environment temperature
of PC dike of PC-type LNG tank.
[0077] The average PBS (Pearlite Block Size) of the wire rod was obtained by the following
procedures. At first, average values (primary average values) of an equivalent circle
diameter of a pearlite block in 300µm × 180µm of fields of view in each of five area
of
- (1) a surface part (an area of which a depth from a surface of the wire rod was 30µm),
- (2) a 1/4D part (an area of which a depth from the surface of the wire rod was 1/4
of a diameter D of the wire rod),
- (3) a center part,
- (4) a 3/4D part (an area of which a depth from the surface of the wire rod was 3/4
of a diameter D of the wire rod, i.e. an area opposite to the (2) with respect to
the center part of the wire rod), and
- (5) an opposite surface part (i.e. an area opposite to the (1) with respect to the
center part of the wire rod),
were measured by using the EBSD device. Then, the average value (secondary average
value) of the each primary average values was calculated. The secondary average value
was assumed as the average PBS in the cross section perpendicular to the wire rod
axial direction. During measuring with EBSD device, a boundary of adjacent two pearlites
between which a difference in crystal orientation was 9° or higher was judged as a
pearlite block boundary.
[0078] The number density of the coarse pearlite blocks of the wire rod was obtained by
the following procedures. At first, number densities of the pearlite block having
40µm or more of grain size in 300µm × 180µm of fields of view in each of five area
of
- (1) a surface part (an area of which a depth from a surface of the wire rod was 30µm),
- (2) a 1/4D part (an area of which a depth from the surface of the wire rod was 1/4
of a diameter D of the wire rod),
- (3) a center part,
- (4) a 3/4D part (an area of which a depth from the surface of the wire rod was 3/4
of a diameter D of the wire rod, i.e. an area opposite to the (2) with respect to
the center part of the wire rod), and
- (5) an opposite surface part (i.e. an area opposite to the (1) with respect to the
center part of the wire rod),
were measured by using the EBSD device. Then, the average value of the each number
densities was calculated. The average value was assumed as the number density of the
pearlite blocks having 40µm or more of grain size in the cross section perpendicular
to the wire rod axial direction.
[Table 1-1]
No |
CHEMICAL COMPOSITION |
UNIT: mass% |
C |
Si |
Mn |
P |
S |
Al |
Ti |
B |
N |
Cr |
V |
S1 |
0.70 |
0.80 |
0.76 |
0.017 |
0.010 |
0.020 |
0.038 |
0.0024 |
0.0031 |
0.50 |
- |
S2 |
0.82 |
0.85 |
0.72 |
0.015 |
0.010 |
0.060 |
0.040 |
0.0037 |
0.0036 |
1.00 |
- |
S3 |
0.88 |
0.90 |
0.72 |
0.008 |
0.006 |
- |
0.048 |
- |
0.0047 |
- |
- |
S4 |
0.88 |
1.00 |
0.73 |
0.006 |
0.009 |
0.025 |
0.005 |
0.0035 |
0.0041 |
0.50 |
0.320 |
S5 |
0.90 |
0.90 |
0.80 |
0.009 |
0.007 |
0.042 |
0.010 |
0.0019 |
0.0060 |
0.50 |
0.310 |
S6 |
0.85 |
0.85 |
0.90 |
0.010 |
0.010 |
0.032 |
- |
0.0020 |
0.0045 |
- |
0.400 |
S7 |
0.90 |
0.85 |
0.72 |
0.012 |
0.000 |
0.033 |
0.025 |
0.0040 |
0.0035 |
0.60 |
- |
S8 |
0.87 |
1.30 |
0.70 |
0.015 |
0.005 |
0.040 |
0.035 |
0.0036 |
0.0025 |
- |
- |
S9 |
0.87 |
0.95 |
0.71 |
0.015 |
0.006 |
0.060 |
- |
0.0028 |
0.0036 |
- |
- |
S10 |
0.87 |
0.96 |
0.74 |
0.011 |
0.009 |
0.060 |
- |
- |
0.0025 |
- |
0.500 |
S11 |
0.87 |
0.98 |
0.75 |
0.020 |
0.007 |
- |
0.015 |
0.0030 |
0.0042 |
0.66 |
- |
S12 |
0.90 |
1.30 |
0.60 |
0.016 |
0.009 |
0.005 |
0.011 |
0.0029 |
0.0036 |
0.56 |
- |
S13 |
0.90 |
0.82 |
0.70 |
0.009 |
0.008 |
0.035 |
0.005 |
- |
0.0039 |
- |
- |
S14 |
0.90 |
0.82 |
0.70 |
0.009 |
0.008 |
- |
- |
0.0035 |
- |
- |
- |
S15 |
0.90 |
0.85 |
0.74 |
0.007 |
0.010 |
0.028 |
0.023 |
0.0033 |
0.0029 |
0.80 |
0.400 |
S16 |
0.90 |
0.85 |
0.74 |
0.007 |
0.010 |
0.028 |
0.023 |
0.0033 |
0.0029 |
0.80 |
0.400 |
S17 |
0.70 |
0.85 |
0.35 |
0.020 |
0.022 |
0.005 |
- |
- |
- |
- |
- |
S18 |
0.82 |
0.75 |
0.81 |
0.022 |
0.019 |
0.030 |
- |
- |
- |
- |
- |
S19 |
0.50 |
0.80 |
0.76 |
0.017 |
0.010 |
0.020 |
0.038 |
0.0024 |
0.0031 |
0.50 |
- |
S20 |
1.03 |
0.85 |
0.74 |
0.007 |
0.010 |
0.028 |
0.023 |
0.0033 |
0.0029 |
0.80 |
0.400 |
S21 |
0.92 |
0.91 |
0.75 |
0.035 |
0.023 |
0.033 |
- |
- |
- |
- |
- |
S22 |
0.82 |
1.38 |
0.72 |
0.015 |
0.010 |
0.060 |
0.040 |
0.0037 |
0.0036 |
1.00 |
- |
S23 |
0.82 |
0.85 |
1.10 |
0.015 |
0.010 |
0.060 |
0.040 |
0.0037 |
0.0036 |
1.00 |
- |
S24 |
0.82 |
0.85 |
0.30 |
0.015 |
0.010 |
0.060 |
0.040 |
0.0037 |
0.0036 |
1.00 |
- |
S25 |
0.82 |
0.85 |
0.72 |
0.042 |
0.010 |
0.060 |
0.040 |
0.0037 |
0.0036 |
1.00 |
- |
S26 |
0.82 |
0.85 |
0.72 |
0.015 |
0.038 |
0.060 |
0.040 |
0.0037 |
0.0036 |
1.00 |
- |
S27 |
0.82 |
0.85 |
0.72 |
0.015 |
0.010 |
0.120 |
0.040 |
0.0037 |
0.0036 |
1.00 |
- |
S28 |
0.82 |
0.85 |
0.72 |
0.015 |
0.010 |
0.060 |
0.120 |
0.0037 |
0.0036 |
1.00 |
- |
S29 |
0.82 |
0.85 |
0.72 |
0.015 |
0.010 |
0.060 |
0.040 |
0.0055 |
0.0036 |
1.00 |
- |
S30 |
0.82 |
0.85 |
0.72 |
0.015 |
0.010 |
0.001 |
0.040 |
0.0037 |
0.0036 |
1.00 |
- |
S31 |
0.82 |
0.85 |
0.72 |
0.015 |
0.010 |
0.060 |
0.001 |
0.0037 |
0.0036 |
1.00 |
- |
S32 |
0.82 |
0.85 |
0.72 |
0.015 |
0.010 |
0.060 |
0.040 |
0.0002 |
0.0036 |
1.00 |
- |
S33 |
0.82 |
0.85 |
0.72 |
0.015 |
0.010 |
0.060 |
0.040 |
0.0037 |
0.0036 |
1.50 |
- |
S34 |
0.82 |
0.85 |
0.72 |
0.015 |
0.010 |
0.060 |
0.040 |
0.0037 |
0.0036 |
1.00 |
0.620 |
S35 |
0.82 |
0.85 |
0.72 |
0.015 |
0.010 |
0.060 |
0.040 |
0.0037 |
0.0036 |
1.00 |
- |
S36 |
0.82 |
0.85 |
0.72 |
0.015 |
0.010 |
0.060 |
0.040 |
0.0037 |
0.0036 |
1.00 |
- |
S37 |
0.82 |
0.85 |
0.72 |
0.015 |
0.010 |
0.060 |
0.040 |
0.0037 |
0.0036 |
1.00 |
- |
S38 |
0.82 |
0.85 |
0.72 |
0.015 |
0.010 |
0.060 |
0.040 |
0.0037 |
0.0036 |
1.00 |
- |
S39 |
0.82 |
0.85 |
0.72 |
0.015 |
0.010 |
0.060 |
0.040 |
0.0037 |
0.0036 |
1.00 |
- |
S40 |
0.82 |
0.85 |
0.72 |
0.015 |
0.010 |
0.060 |
0.040 |
0.0037 |
0.0036 |
1.00 |
- |
S41 |
0.82 |
0.85 |
0.72 |
0.015 |
0.010 |
0.060 |
0.040 |
0.0037 |
0.0036 |
1.00 |
- |
UNDERLINED VALUE IS OUT OF RANGE OF PRESENT INVENTION |
[Table 1-2]
No |
HEATING TEMPERATURE BEFORE ROUGH-ROLLING |
FINISH-ROLLING TEMPERATURE |
STRAIN RATE IN THE FINISH-WIRE-ROLLING |
log 10Z |
COILING TEMPERATURE |
COOLING RATE |
REMARKS |
°C |
°C |
s-1 |
°C |
°C/s |
S1 |
950 |
750 |
607 |
16.5 |
730 |
15 |
|
S2 |
950 |
800 |
607 |
15.8 |
750 |
15 |
|
S3 |
960 |
750 |
607 |
16.5 |
730 |
22 |
|
S4 |
970 |
800 |
607 |
15.8 |
780 |
20 |
|
S5 |
980 |
800 |
607 |
15.8 |
790 |
15 |
|
S6 |
980 |
850 |
607 |
15.2 |
800 |
16 |
|
S7 |
1000 |
900 |
607 |
14.7 |
790 |
17 |
|
S8 |
1000 |
850 |
607 |
15.2 |
785 |
15 |
|
S9 |
1000 |
850 |
607 |
15.2 |
800 |
15 |
EXAMPLE |
S10 |
1020 |
850 |
607 |
15.2 |
790 |
20 |
S11 |
1030 |
800 |
607 |
15.8 |
790 |
20 |
|
S12 |
1030 |
800 |
607 |
15.8 |
795 |
22 |
|
S13 |
1040 |
750 |
607 |
16.5 |
730 |
20 |
|
S14 |
1040 |
750 |
607 |
16.5 |
730 |
20 |
|
S15 |
1040 |
900 |
607 |
14.7 |
830 |
25 |
|
S16 |
1040 |
900 |
607 |
14.7 |
830 |
25 |
|
S17 |
1080 |
1050 |
371 |
13.2 |
880 |
5 |
|
S18 |
1080 |
1000 |
371 |
13.6 |
850 |
10 |
|
S19 |
950 |
750 |
371 |
16.3 |
730 |
15 |
|
S20 |
1040 |
900 |
371 |
14.5 |
800 |
25 |
|
S21 |
1100 |
1100 |
371 |
12.8 |
900 |
12 |
|
S22 |
950 |
800 |
607 |
15.8 |
750 |
15 |
|
S23 |
950 |
800 |
607 |
15.8 |
750 |
15 |
|
S24 |
950 |
800 |
607 |
15.8 |
750 |
15 |
|
S25 |
950 |
800 |
607 |
15.8 |
750 |
15 |
|
S26 |
950 |
800 |
607 |
15.8 |
750 |
15 |
|
S27 |
950 |
800 |
607 |
15.8 |
750 |
15 |
|
S28 |
950 |
800 |
607 |
15.8 |
750 |
15 |
|
S29 |
950 |
800 |
607 |
15.8 |
750 |
15 |
|
S30 |
950 |
800 |
607 |
15.8 |
750 |
15 |
COMPARATIVE EXAMPLE |
S31 |
950 |
800 |
607 |
15.8 |
750 |
15 |
S32 |
950 |
800 |
607 |
15.8 |
750 |
15 |
S33 |
950 |
800 |
607 |
15.8 |
750 |
15 |
|
S34 |
950 |
800 |
607 |
15.8 |
750 |
15 |
|
S35 |
1150 |
800 |
607 |
15.8 |
750 |
15 |
|
S36 |
950 |
720 |
607 |
16.9 |
750 |
15 |
|
S37 |
950 |
1150 |
607 |
12.6 |
750 |
15 |
|
S38 |
950 |
800 |
607 |
15.8 |
890 |
15 |
|
S39 |
950 |
800 |
607 |
15.8 |
750 |
7 |
|
S40 |
950 |
950 |
607 |
14.2 |
750 |
15 |
|
S41 |
950 |
900 |
42 |
13.5 |
750 |
15 |
|
UNDERLINED VALUE IS OUT OF RANGE OF PRESENT INVENTION
FINAL DIAMETER: 12mm
ACTIVATION ENERGY OF PLASTIC DEFORMATION: 63800cal/mol |

[0079] The heating temperature, the finishing temperature, and the coiling temperature of
the examples were within the adequate temperature range. Therefore, the pearlite block
of the example was refined and the average PBS and the number density of the coarse
PB of the example were controlled in the adequate level. On the other hand, the average
PBS and the number density of the coarse PB of the comparative examples of which the
heating temperature, the finishing temperature, and/or the coiling temperature were
higher than the adequate temperature range were out of range defined by the present
invention. The examples demonstrated better property than the comparative examples
in low-temperature strength, low-temperature toughness, and room-temperature toughness.
In example S36, the finish-rolling temperature was lower than the adequate temperature
range, and thus, mill load increased to prevent rolling from performing.
[0080] Figure 5A shows SEM picture of the pearlite block of the example and Figure 5B shows
SEM picture of the pearlite block of the comparative example. It could be found from
the SEM pictures that the grain size of the pearlite block of the example was smaller
than the grain size of the pearlite block of the comparative example.
[0081] Figure 6 shows a result of tensile test at -40°C of the example (No. S6) and the
comparative example (No. S17). It could be found that the elongation of the example
was higher and better than the elongation of the comparative example in low-temperature
atmosphere of -40°C. In addition, it could be found from Table 2 that the elongation
of the example tended to be higher than the elongation of the comparative example.
It was assumed that the difference in elongation was caused by the difference in the
grain size of the pearlite block shown in Figure 5A and Figure 5B.
[0082] Next, examples by a method for manufacturing with DLP method will be described hereinafter.
[0083] At first, molten steel having chemical composition shown in Table 3 was continuously
casted so as to be a cast bloom of 300mm × 500mm, and the cast bloom was rolled so
as to be a steel billet of 122mm square. Then, the steel billet was heated to a heating
temperature shown in Table 3 and rolled, coiled and heat treated using molten salt
under a condition shown in the Table 3 to obtain a wire rod of 12mmϕ. No. D1 to D16
and No. D30 to D36 were manufactured with a heat treatment (direct heat treatment)
in which they were immersed into the molten salt without reheating after coiling.
No. D17 to D29 were coiled under conditions shown in the Table 3, and then, subjected
to a heat treatment (offline heat treatment) in which they were reheated to 950°C
and subjected to lead patenting treatment.
[0084] Tensile strength at -40°C, elongation at -40°C, and impact value at -40°C of the
above-described wire rods were obtained. The test methods for obtaining the values
were same to each test methods performed to the above-described No. S1 to No. S41.
In addition, charpy impact test at room temperature was performed to the above-described
wire rods to obtain impact value of the wire rods at the room temperature. The method
for performing the charpy impact test at the room temperature was same to the above-described
method for performing the charpy impact test at -40°C except test temperature. The
average PBS and the number density of the coarse pearlite blocks of the above-described
wire rod were measured.
[Table 3-1]
|
CHEMICAL COMPOSITION |
HEATING TEMPERATURE BEFORE WIRE ROD ROLLING |
COILING TEMPERATURE |
ONLINE HEAT TREATMENT TEMPERATURE |
REMARKS |
No |
UNIT: mass% |
|
C |
Si |
Mn |
P |
s |
Al |
Ti |
B |
N |
Cr |
V |
°C |
°C |
°C |
|
D1 |
0.60 |
0.80 |
0.76 |
0.017 |
0.010 |
0.020 |
0.038 |
0.0024 |
0.0031 |
- |
- |
950 |
750 |
500 |
|
D2 |
0.82 |
0.85 |
0.72 |
0.015 |
0.010 |
0.060 |
0.040 |
0.0037 |
0.0036 |
- |
0.120 |
950 |
750 |
500 |
|
D3 |
0.88 |
0.90 |
0.72 |
0.008 |
0.006 |
0.030 |
0.048 |
0.0039 |
0.0047 |
- |
- |
960 |
780 |
520 |
|
D4 |
0.88 |
1.00 |
0.73 |
0.006 |
0.009 |
0.025 |
0.005 |
0.0035 |
0.0041 |
0.27 |
0.320 |
970 |
780 |
520 |
|
D5 |
0.90 |
0.90 |
0.80 |
0.009 |
0.007 |
0.042 |
0.010 |
- |
0.0060 |
0.23 |
0.210 |
980 |
790 |
520 |
|
D6 |
0.92 |
0.85 |
0.90 |
0.010 |
0.010 |
0.032 |
0.018 |
0.0020 |
0.0045 |
- |
0.030 |
980 |
800 |
520 |
|
D7 |
0.92 |
0.85 |
0.72 |
0.012 |
0.000 |
0.033 |
- |
0.0040 |
0.0025 |
0.15 |
- |
1000 |
790 |
550 |
EXAMPLE |
D8 |
0.95 |
1.30 |
0.70 |
0.015 |
0.005 |
- |
0.035 |
0.0036 |
0.0035 |
- |
- |
1000 |
785 |
550 |
D9 |
0.95 |
0.95 |
0.71 |
0.015 |
0.006 |
0.085 |
0.031 |
0.0028 |
0.0036 |
- |
- |
1000 |
800 |
550 |
D10 |
0.98 |
0.96 |
0.74 |
0.011 |
0.009 |
0.060 |
- |
- |
0.0025 |
- |
0.120 |
1020 |
790 |
550 |
|
D11 |
0.98 |
0.98 |
0.75 |
0.013 |
0.007 |
0.032 |
- |
0.0030 |
0.0042 |
0.16 |
- |
1030 |
790 |
560 |
|
D12 |
0.98 |
1.00 |
0.40 |
0.016 |
0.009 |
0.005 |
0.011 |
0.0029 |
0.0036 |
0.41 |
- |
1030 |
795 |
560 |
|
D13 |
1.00 |
0.82 |
0.38 |
0.009 |
0.008 |
0.035 |
0.005 |
- |
0.0039 |
- |
- |
1040 |
800 |
575 |
|
D14 |
1.18 |
0.85 |
0.35 |
0.020 |
0.010 |
0.028 |
0.023 |
0.0033 |
0.0029 |
0.48 |
0.010 |
1040 |
800 |
575 |
|
D15 |
0.98 |
0.98 |
0.75 |
0.013 |
0.007 |
0.032 |
0.040 |
0.0030 |
0.0042 |
0.16 |
- |
1030 |
790 |
560 |
|
016 |
1.00 |
0.85 |
0.35 |
0.020 |
0.010 |
- |
- |
0.0038 |
0.0029 |
0.48 |
0.010 |
1040 |
800 |
575 |
|
[Table 3-2]
No |
CHEMICAL COMPOSITION |
HEATING TEMPERATURE BEFORE WIRE ROD ROLLING |
COILING TEMPERATURE |
ONLINE HEAT TREATMENT TEMPERATURE |
REMARKS |
UNIT: mass% |
|
C |
Si |
Mn |
P |
S |
Al |
Ti |
B |
N |
Cr |
V |
°C |
°C |
°C |
|
D17 |
0.64 |
0.80 |
0.76 |
0.017 |
0.010 |
0.020 |
0.038 |
0.0024 |
0.0031 |
- |
- |
950 |
750 |
500 |
|
D18 |
0.82 |
0.32 |
0.72 |
0.015 |
0.010 |
0.060 |
0.040 |
0.0037 |
0.0036 |
- |
0.120 |
950 |
750 |
500 |
|
D19 |
0.88 |
0.63 |
0.72 |
0.008 |
0.006 |
0.030 |
0.048 |
0.0039 |
0.0047 |
- |
- |
960 |
780 |
520 |
|
D20 |
0.83 |
0.85 |
0.35 |
0.020 |
0.022 |
0.024 |
0.110 |
- |
0.0045 |
0.22 |
- |
1080 |
850 |
560 |
|
D21 |
0.87 |
0.75 |
0.81 |
0.022 |
0.019 |
0.030 |
0.160 |
- |
0.0040 |
- |
0.520 |
1080 |
850 |
565 |
|
D22 |
0.88 |
0.91 |
0.75 |
0.035 |
0.023 |
- |
- |
- |
- |
- |
- |
1100 |
850 |
550 |
COMPARATIVE EXAMPLE |
D23 |
0.91 |
0.92 |
0.73 |
0.018 |
0.032 |
0.041 |
0.060 |
0.0030 |
0.0035 |
0.32 |
- |
1100 |
850 |
550 |
D24 |
0.92 |
0.85 |
0.25 |
0.023 |
0.026 |
0.120 |
0.210 |
0.0025 |
0.0045 |
0.61 |
- |
1120 |
850 |
563 |
D25 |
0.95 |
0.88 |
0.60 |
0.032 |
0.011 |
0.027 |
0.340 |
- |
0.0051 |
0.41 |
- |
1120 |
860 |
570 |
|
D26 |
0.98 |
1.31 |
0.45 |
0.025 |
0.015 |
0.023 |
0.110 |
- |
0.0023 |
0.32 |
0.100 |
1130 |
860 |
570 |
|
D27 |
0.95 |
1.30 |
0.70 |
0.015 |
0.005 |
- |
0.035 |
0.0036 |
0.0015 |
- |
- |
1130 |
850 |
570 |
|
D28 |
1.05 |
1.20 |
0.85 |
0.027 |
0.019 |
0.027 |
0.190 |
0.0054 |
0.0037 |
- |
0.250 |
1130 |
860 |
575 |
|
D29 |
1.10 |
0.96 |
0.79 |
0.019 |
0.011 |
0.025 |
0.230 |
- |
0.0073 |
- |
0.330 |
1135 |
860 |
580 |
|
No |
CHEMICAL COMPOSITION |
HEATING TEMPERATURE BEFORE WIRE ROD ROLLING |
COILING TEMPERATURE |
ONLINE HEAT TREATMENT TEMPERATURE |
REMARKS |
UNIT: mass% |
|
C |
Si |
Mn |
P |
S |
Al |
Ti |
B |
N |
Cr |
V |
°C |
°C |
°C |
|
D30 |
0.50 |
0.85 |
0.72 |
0.015 |
0.010 |
0.060 |
0.040 |
0.0037 |
0.0036 |
- |
0.120 |
950 |
750 |
500 |
|
D31 |
1.25 |
0.90 |
0.72 |
0.008 |
0.006 |
0.030 |
0.048 |
0.0039 |
0.0047 |
- |
- |
960 |
780 |
520 |
|
D32 |
1.05 |
1.20 |
0.85 |
0.027 |
0.019 |
0.027 |
0.190 |
0.0054 |
0.0037 |
- |
0.250 |
1135 |
860 |
420 |
|
D33 |
0.95 |
1.30 |
0.70 |
0.015 |
0.005 |
- |
0.035 |
0.0036 |
0.0015 |
- |
- |
1130 |
850 |
450 |
COMPARATIVE EXAMPLE |
D34 |
0.88 |
0.90 |
0.72 |
0.008 |
0.006 |
0.030 |
0.048 |
0.0039 |
0.0047 |
- |
- |
1080 |
780 |
520 |
D35 |
0.90 |
0.90 |
0.80 |
0.009 |
0.007 |
0.042 |
0.010 |
- |
0.0060 |
0.23 |
0.210 |
980 |
735 |
520 |
D36 |
0.90 |
0.90 |
0.80 |
0.009 |
0.007 |
0.042 |
0.010 |
- |
0.0060 |
0.23 |
0.210 |
980 |
880 |
520 |
|
D37 |
0.92 |
0.24 |
0.72 |
0.012 |
0.000 |
0.033 |
- |
0.0040 |
0.0025 |
0.15 |
- |
1000 |
790 |
550 |
|
D38 |
0.95 |
1.30 |
0.20 |
0.015 |
0.005 |
- |
0.035 |
0.0036 |
0.0035 |
- |
- |
1000 |
785 |
550 |
|
UNDERLINED VALUE IS OUT OF RANGE OF PRESENT INVENTION |
[Table 4-1]
No |
AVERAGE PBS |
NUMBER DENSITY OF COARSE PB |
TENSILE STRENGTH AT -40°C |
ELONGATION AT -40°C |
CHARPY IMPACT VALUE AT -40°C |
CHARPY IMPACT VALUE AT ROOM TEMPERATURE |
REMARKS |
µm |
|
MPa |
% |
J |
J |
D1 |
15 |
0 |
1201 |
18.0 |
15.0 |
25.0 |
|
D2 |
18 |
0 |
1265 |
17.8 |
14.7 |
24.0 |
|
D3 |
19 |
0 |
1295 |
17.1 |
14.0 |
23.9 |
|
D4 |
18 |
0 |
1380 |
16.8 |
13.0 |
23.4 |
|
D5 |
15 |
0 |
1390 |
16.6 |
13.2 |
23.0 |
|
D6 |
16 |
0 |
1430 |
16.2 |
13.8 |
23.0 |
|
D7 |
17 |
0 |
1410 |
16.3 |
13.5 |
22.5 |
|
D8 |
15 |
0 |
1490 |
15.9 |
13.6 |
21.0 |
EXAMPLE |
D9 |
18 |
0 |
1460 |
15.6 |
14.0 |
22.0 |
D10 |
20 |
0 |
1530 |
15.5 |
13.2 |
22.0 |
|
D11 |
19 |
0 |
1540 |
14.8 |
13.6 |
21.5 |
|
D12 |
18 |
0 |
1530 |
14.5 |
13.0 |
21.0 |
|
D13 |
20 |
20 |
1540 |
13.4 |
13.2 |
20.3 |
|
D14 |
23 |
18 |
1580 |
13.1 |
13.0 |
20.0 |
|
D15 |
22 |
0 |
1530 |
13.7 |
13.0 |
21.0 |
|
D16 |
23 |
0 |
1542 |
13.5 |
13.0 |
20.0 |
|
[Table 4-2]
No |
AVERAGE PBS |
NUMBER DENSITY OF COARSE PB |
TENSILE STRENGTH AT -40°C |
ELONGATION AT -40°C |
CHARPY IMPACT VALUE AT -40°C |
CHARPY IMPACT VALUE AT ROOM TEMPERATURE |
REMARKS |
µm |
|
MPa |
% |
J |
J |
D17 |
28 |
44 |
1100 |
9.7 |
10.1 |
17.0 |
|
D18 |
27 |
51 |
1210 |
9.5 |
10.0 |
15.0 |
|
D19 |
28 |
50 |
1230 |
9.2 |
9.5 |
16.0 |
|
D20 |
30 |
79 |
1255 |
8.7 |
9.0 |
16.0 |
|
D21 |
35 |
120 |
1280 |
8.6 |
8.6 |
15.3 |
|
D22 |
38 |
60 |
1310 |
8.0 |
8.5 |
15.1 |
COMPARATIVE EXAMPLE |
D23 |
40 |
140 |
1420 |
7.0 |
7.0 |
15.1 |
D24 |
44 |
160 |
1400 |
7.5 |
7.5 |
14.7 |
D25 |
48 |
180 |
1480 |
6.0 |
7.2 |
14.6 |
|
D26 |
34 |
120 |
1580 |
5.4 |
7.0 |
14.3 |
|
D27 |
42 |
100 |
1525 |
5.6 |
6.9 |
15.0 |
|
D28 |
35 |
170 |
1540 |
5.4 |
6.5 |
14.1 |
|
D29 |
45 |
160 |
1570 |
5.4 |
6.0 |
14.0 |
|
No |
PBS |
NUMBER DENSITY OF COARSE PB |
TENSILE STRENGTH AT -40°c |
ELONGATION AT -40°C |
CHARPY IMPACT VALUE AT -40°C |
CHARPY IMPACT VALUE AT ROOM TEMPERATURE |
REMARKS |
µm |
|
MPa |
% |
J |
J |
D30 |
21 |
20 |
1010 |
11 |
18.2 |
22.0 |
|
D31 |
23 |
23 |
1590 |
5.1 |
3.0 |
9.0 |
|
D32 |
41 |
40 |
1310 |
6.3 |
6.2 |
14.0 |
|
D33 |
39 |
60 |
1300 |
6.9 |
6.0 |
14.3 |
COMPARATIVE EXAMPLE |
D34 |
25 |
56 |
1375 |
6.2 |
8.5 |
14.0 |
D35 |
30 |
65 |
1250 |
5.1 |
7.8 |
13.0 |
D36 |
45 |
70 |
1385 |
9.2 |
9.8 |
15.2 |
|
D37 |
15 |
0 |
1380 |
3 |
4.2 |
9.5 |
|
D38 |
39 |
52 |
1490 |
4.9 |
5.3 |
13.2 |
|
UNDERLINED VALUE IS OUT OF RANGE OF PRESENT INVENTION |
[0085] No. D1 to D16 of the Table 3 were examples satisfying the condition according to
the present invention. On the other hand, No. D17 to D38 of the Table 4 were comparative
examples which did not satisfy the conditions according to the present invention.
Although the grain size of the pearlite block and the number density of the coarse
PB of the example were controlled to the adequate level, the grain size of the pearlite
block and the number density of the coarse PB of the comparative example were out
of the range defined by the present invention. The examples demonstrated more excellent
low-temperature strength, low-temperature toughness, and room-temperature toughness
as compared with the comparative examples.
[0086] Figure 7A shows SEM picture of the pearlite block of the example and Figure 7B shows
SEM picture of the pearlite block of the comparative example. It could be found from
the SEM pictures that the grain size of the pearlite block of the example was clearly
different from that of the comparative example.
[0087] Figure 8 shows a relationship between the grain size of the pearlite block (µm) and
the impact value based on the impact value shown in Table 4. It could be found from
the Figure 8 that the impact value of the example (PBS: 15 to 23µm) was higher than
the impact value of the comparative example (PBS: 30 to 45µm) in both of room temperature
and -40°C.
[0088] Figure 9A and Figure 9B show SEM observation result of the fracture surface of the
charpy impact test piece of the example and comparative example. Figure 9A shows fracture
facet of the example and Figure 9B shows fracture facet of the comparative example.
The fracture facet of the example was finer than the fracture facet of the comparative
example. This indicates that the example had more excellent toughness than the comparative
example. In view of the point, the effect of refining PBS could be found.
[0089] Accordingly, it was found that the toughness of the example was higher than the toughness
of the comparative example at both of room temperature and the environment of -40°C,
to which the wire rod was exposed when the wire rod was used as additional PC of LNG
tank.
[Industrial Applicability]
[0090] According to the present invention, a wire rod for PC steel stranded wire which is
used as tendon of PC dike of PC-type LNG tank and which has more excellent elongation
at about -40°C as compared with the conventional material can be provided by reducing
grain size of pearlite block. Therefore, the present invention contributes to enhancing
reliability of the PC steel stranded wire, which is a member constructing equipments
concerning LNG tank which is much in demand these days, under low-temperature usage
environment, and thus, the present invention has significant industrial applicability.
[Brief Description of the Reference Symbols]
[0091]
- 1:
- wire rod
- 2:
- 2mm U-notch charpy impact test piece
- 3:
- 2mm U-notch