Technical Field
[0001] The present invention generally relates to steel plates (thick steel plates) to be
applied to welded structures such as bridges, high-rise buildings, ships (marine vessels),
and line pipes. More specifically, the present invention relates to a steel plate
having excellent toughness in a heat affected zone after high heat input welding.
The heat affected zone is hereinafter also simply referred to as HAZ.
Background Art
[0002] Welded structures such as bridges, high-rise buildings, ships, and line pipes have
recently had larger and larger sizes. These welded structures have been increasingly
made from steel plates having a thickness of 50 mm or more. This requires welding
of such steel plates having a thickness of 50 mm or more. Under these circumstances,
demands have been made to provide high heat input welding for better welding working
efficiency.
[0003] The HAZ upon high heat input welding, however, is held in the high-temperature austenite
(y) region for a long time upon heating and then gradually cooled. This often causes
the coarsening of the microstructure typically by growth of austenite grains upon
heating and formation of coarse ferrite (a) grains during the cooling process. This
in turn causes the HAZ to have lower toughness upon high heat input welding. To prevent
this, demands have been made to develop a technique for maintaining the toughness
of HAZ stably at high level upon high heat input welding. The toughness of HAZ is
hereinafter also referred to as "HAZ toughness".
[0004] Proposed techniques to ensure the HAZ toughness at certain level include techniques
relating to austenite grain growth pinning by inclusion particles, and to microstructure
refinement by intragranular ferrite formation occurring at such inclusion particles.
The inclusions are exemplified by oxides, nitrides, and sulfides. Such proposed techniques
include techniques described in Patent Literature (PTL) and PTL 2. Specifically, PTL
1 and PTL 2 disclose that fine titanium nitride particles, when dispersed and precipitated
as austenite grain growth pinning particles in a steel, inhibit the coarsening of
austenite grains formed in the HAZ upon high heat input welding and inhibit the HAZ
toughness from deteriorating. The titanium nitride particles readily disappear with
a higher welding heat input, and there is a need for a special scheme in order to
obtain stable HAZ toughness.
[0005] The present inventors have also proposed a technique of precisely controlling the
size and number (number density) of fine titanium nitride particles so as to improve
HAZ toughness upon high heat input welding in PTL 3. However, the assumed heat input
in this technique is at most 55 kJ/mm, and there is a need for further improvements
so as to support further higher welding heat input.
[0006] PTL 4 to 7 have proposed techniques of utilizing oxide inclusions as austenite grain
growth pinning particles, where the oxide inclusions are stable at high temperatures.
The oxide inclusions, however, are few in number as compared with titanium-containing
nitrides and fail to provide a sufficient pinning effects. The techniques therefore
fail to support high heat input welding sufficiently, and there is a need for still
further improvements.
[0007] Specifically, PTL 4 describes that the presence of oxides containing rare-earth elements
(REM) and/or Zr gives good HAZ properties. However, the assumed heat input in the
technique remains still low, and the technique is not considered to always provide
good HAZ properties upon high heat input welding. PTL 5 describes a technique of using
oxides containing REM and/or Zr as with PTL 4. In this technique, the HAZ toughness
is evaluated as Charpy absorbed energy (Charpy impact energy). It is considered, however,
that not only the average, but also the minimum of this parameter should be maintained
or secured at high level from the viewpoint of material reliability.
[0008] PTL 6 describes a technique of using both oxide inclusions and titanium-containing
inclusions as austenite grain growth pinning particles to give high HAZ toughness.
In the technique in PTL 6, the HAZ toughness is evaluated by a thermal cycle test
that simulates high heat input welding. The test is performed at a highest heating
temperature of 1400°C at which part of titanium-containing nitrides remains. In actual,
however, the highest heating temperature in the HAZ partially becomes as high as greater
than 1450°C, and this still further promotes the disappearance of titanium-containing
nitrides. Accordingly, a high heat input welding test is desirably actually performed
so as to accurately evaluate the HAZ toughness upon high heat input. The present inventors
have proposed a technique using the austenite grain growth pinning effect of fine
oxide inclusions in PTL 7. This technique also utilizes the inhibition of reprecipitation
of fine manganese sulfide particles and requires complicated control of determining
amounts of alloy elements to be added based on the dissolved oxygen amount and dissolved
sulfur amount.
[0009] Independently, exemplary techniques relating to the microstructure refinement due
to intragranular ferrite formation occurring at inclusion particles are as follows.
PTL 8 describes a technique of utilizing MnS (manganese sulfide) and complex oxides
containing Ti and REM. The present inventors have proposed a technique of controlling
the form of inclusions to promote the intragranular ferrite formation in PTL 9. These
techniques have been made on the assumption that inclusions having a low interfacial
energy between intragranular ferrite and the inclusions are effective in intragranular
ferrite formation. However, the techniques have not yet reached sufficient HAZ toughness
upon high heat input. This is because the intragranular ferrite formation is largely
affected also by the interfacial energy between intragranular ferrite and austenite,
and is not sufficiently obtained merely by decreasing the interfacial energy between
intragranular ferrite and inclusions.
[0010] The present inventors have developed a technique to provide high HAZ toughness using
intragranular ferrite formation occurring at oxi-sulfides and have proposed in PTL
10. However, in return for the high HAZ toughness, there is a need for dispersing
relatively large-sized oxi-sulfide particles having a size of 2 µm or more. Thus,
this technique has also not yet reached sufficient HAZ toughness upon high heat input.
Specifically, the technique described in PTL 8 employs a small heat input as assumed;
whereas the techniques described in PTL 9 and PTL 10 provide, in Charpy absorbed energy,
a high average, but a minimum that is susceptible to improvements under present circumstances.
[0011] In addition, the present inventors have proposed techniques of dispersing oxides
having a controlled microstructure to give high HAZ toughness in PTL 11 and PTL 12.
These techniques actually provide steel plates having excellent heat affected zone
toughness, but are still susceptible to improvements upon production.
[0012] The technique described in PTL 11 controls the amount of Ca to be added based on
the amount of dissolved oxygen before the addition of Ca so as to provide predetermined
oxide particle form. This technique, however, should be performed so that the time
from the Ti addition to the Ca addition falls within the range of 3 to 20 minutes
and may increase the operator's burden. The technique described in PTL 12 requires
holding of the work for a time of 40 minutes to 90 minutes in a period of time from
the Ca addition to casting (pouring) and is still susceptible to improvements in productivity.
Citation List
Patent Literature
Summary of Invention
Technical Problem
[0014] The present invention has been made under the circumstances of the conventional techniques
and has an object to provide a steel plate that can have not only a higher average,
but also a higher minimum charpy impact value in HAZ toughness even upon high heat
input welding, has excellent heat affected zone toughness, and exhibits excellent
productivity.
Solution to Problem
[0015] The present invention provides, according to a first embodiment, a steel plate having
excellent heat affected zone toughness. The steel plate contains, in mass percent,
C in a content of 0.03% to 0.12%, Si in a content of 0.10% to 0.25%, Mn in a content
of 1.0% to 2.0%, P in a content of 0.03% or less (excluding 0%), S in a content of
0.015% or less (excluding 0%), Al in a content of 0.004% to 0.05%, Ti in a content
of 0.010% to 0.050%, at least one rare-earth element (REM) in a content of 0.0003%
to 0.02%, Zr in a content of 0.0003% to 0.02%, Ca in a content of 0.0005% to 0.010%,
and N in a content of 0.002% to 0.010% with the remainder being iron and inevitable
impurities. The steel plate includes oxide particles that contain constituent elements
excluding oxygen in contents, in mass percent, meeting conditions as follows: 2% <
Ti < 40%, 5% < Al < 30%; 5% < Ca < 40%, 5% < REM < 50%, 2% < Zr < 30%, and 1.0 ≤ REM/Zr.
Of the oxide particles, oxide particles having an equivalent circle diameter of less
than 2 µm are present in a number density of 300 or more per square millimeter, and
oxide particles having an equivalent circle diameter of 2 µm or more are present in
a number density of 100 or less per square millimeter. The steel plate includes titanium
nitride particles. Of the titanium nitride particles, titanium nitride particles having
an equivalent circle diameter of 1 µm or more are present in a number density of 7
or less per square millimeter, and titanium nitride particles having an equivalent
circle diameter of 20 nm or more are present in a number density of 1.0x 10
6 or more per square millimeter. The steel plate has df and da meeting a condition
specified by the relational expression:

in which the df is defined so that the titanium nitride particles having an equivalent
circle diameter of 20 nm or more are classified into ranges of equivalent Circle diameter
of from 20 nm up to 500 nm every 5 nm in an increasing order, in which particles in
each of the ranges have an equivalent circle diameter of (di-5) to less than di, where
di is 25, 30, 35,...500, and the di in a range having a largest number of titanium
nitride particles present in the range is defined as the df. The da represents an
average equivalent circle diameter of the titanium nitride particles having an equivalent
circle diameter of 20 nm to less than 500 nm.
[0016] As used above and hereinafter the term "equivalent circle diameter" refers to the
diameter of an assumed circle having an equivalent area to the size (area) of an oxide
particle or a titanium nitride particle in question. The equivalent circle diameter
may be determined by observation under a transmission electron microscope (TEM) or
a scanning electron microscope (SEM).
[0017] According to a second embodiment, the steel plate having excellent heat affected
zone toughness may include specific oxides in a number density of 300 or more per
square millimeter, where the specific oxides include constituent elements excluding
oxygen in contents, in mass percent, meeting conditions as follows: 2% < Ti < 40%,
5% < Al < 30%, 5% < Ca < 40%, 5% < REM < 50%, 2% < Zr < 30%, and 1.5 ≤ REM/Zr.
[0018] The steel plate having excellent heat affected zone toughness, according to a third
embodiment, may further contain at least one selected from the group consisting of,
in mass percent, Ni in a content of 0.05% to 1.50%, Cu in a content of 0.05% to 1.50%,
Cr in a content of 0.05% to 1.50%, Mo in a content of 0.05% to 1.50%, Nb in a content
of 0.002% to 0.10%, V in a content of 0.002% to 0.10%, and B in a content of 0.0005%
to 0.0050%. Advantageous Effects of Invention
[0019] The present invention provides a steel plate that can have a higher average and a
higher minimum in HAZ toughness not only upon low to moderate heat input welding,
but also even upon high heat input welding, has such excellent heat affected zone
toughness, and still exhibits excellent productivity.
Description of Embodiments
[0020] The present inventors have made searches for ways to allow a steel plate to have
better HAZ toughness upon high heat input under production conditions with relatively
high productivity. As a result, the present inventors have found as follows. Assume
that intragranular ferrite formation occurring at oxides is ensured, coarse titanium
nitride particles acting as an inhibitory factor to HAZ toughness are inhibited to
be formed, and titanium nitride particles are dispersed in an appropriately controlled
form. This allows a steel plate to have productivity and HAZ toughness upon high heat
input both at satisfactory levels. Specifically, the present inventors have findings
as follows. Assume that the oxides are controlled appropriately in their chemical
compositions. This ensures intragranular ferrite formation. Further assume that the
titanium nitride particles are appropriately controlled in size and number to inhibit
coarsening of prior austenite grains. This enables the refinement of grain-boundary
ferrite grains that are formed at prior austenite grain boundaries. Thus, a steel
plate having excellent HAZ toughness upon high heat input is provided.
[0021] More specifically, the present inventors have verified as follows. Assume that, of
the oxides, those having an equivalent circle diameter of less than 2 µm are dispersed
in a number density of 300 or more per square millimeter, but those having an equivalent
Circle diameter of 2 µm or more are controlled to be dispersed in a number density
of 100 or less per square millimeter. This provides excellent HAZ toughness.
[0022] The present invention has been made based on the above-mentioned findings. The individual
elements and conditions are specified for reasons as follows.
[0023] In the steel plate, oxide particles meeting the conditions of constituent elements
excluding oxygen in contents, in mass percent: 2% < Ti < 40%, 5% < Al < 30%, 5% <
Ca < 40%, 5% < REM < 50%, 2% < Zr < 30%, and 1.0 ≤ REM/Zr, and having an equivalent
circle diameter of less than 2 µm are present in a number density of 300 or more per
square millimeter.
[0024] The majority of oxide particles are controlled to have an equivalent circle diameter
of less than 2 µm. Such fine oxide particles promote intragranular ferrite formation
to improve the HAZ toughness. In contrast, oxide particles having an equivalent circle
diameter of 2 µm or more may lower the barrier energy upon formation of coarse titanium
nitride particles to increase the amount of formed coarse titanium nitride particles.
Oxide particles, if having a chemical composition, in mass percent, not meeting the
conditions of 2% < Ti < 40%, 5% < Al < 30%, 5% < Ca < 40%, 5% < REM < 50%, 2% < Zr
< 30%, and 1.0 ≤ REM/Zr, may fail to contribute to sufficient intragranular ferrite
formation. In a preferred embodiment, the ratio (in mass percent) of REM to Zr in
the oxide particles may be controlled to 1.5 or more. This further reduces the amount
of coarsely formed titanium nitride particles in the surface of the oxide particles
in molten steel to achieve still further excellent HAZ toughness.
[0025] In the steel plate, oxide particles having an equivalent circle diameter of 2 µm
or more are present in a number density of 100 or less per square millimeter.
[0026] Of the oxide particles meeting the chemical composition as above, those having an
equivalent circle diameter of 2 µm or more cause deterioration in HAZ toughness and
are preferably minimized. From this viewpoint, the number density of oxide particles
having an equivalent circle diameter of 2 µm or more is controlled to 100 or less
per square millimeter in the present invention.
[0027] According to an embodiment of the present invention, the form of titanium nitride
(particles) is specified in detail. The titanium nitride inhibits austenite grain
coarsening upon HAZ high-temperature heating, reduces the sizes of grain-boundary
ferrite grains formed during cooling, and thereby contributes to better HAZ toughness.
To sufficiently inhibit austenite grain coarsening, a large number of titanium nitride
particles should naturally be dispersed. In addition to this, the present inventors
have found that the titanium nitride particles are dissolved at a lower dissolution
rate upon HAZ high-temperature heating with more uniformized sizes of the particles;
and that appropriate control of the size and number of the titanium nitride particles
can effectively inhibit austenite grain coarsening even upon high heat input welding.
Specifically, the steel plate, when meeting two conditions as follows, can exhibit
satisfactory HAZ toughness upon high heat input.
[0028] In the first condition, titanium nitride particles having an equivalent circle diameter
of 1 µm or more are controlled to be present in a number density of 7 or less per
square millimeter.
[0029] The titanium nitride particles having an equivalent circle diameter of 1 µm or more,
if present in a number density of greater than 7 per square millimeter, may cause
the steel plate to have inferior HAZ toughness. Such titanium nitride particles have
a rectangular parallelepiped shape, still have remarkably high hardness as compared
with the steel, and cause stress concentration to significantly impair the HAZ toughness.
Accordingly, the coarse titanium nitride particles should be more strictly controlled
as compared with coarse oxide particles.
[0030] In the second condition, titanium nitride particles having an equivalent Circle diameter
of 20 nm or more are present in a number density of 1.0x 10
6 or more per square millimeter.
[0031] The titanium nitride particles having an equivalent circle diameter of 20 nm or more,
if present in a number density of less than 1.0x 10
6 per square millimeter, may fail to sufficiently act as titanium nitride particles
necessary in inhibition of austenite grain coarsening. Ultrafine titanium nitride
particles having an equivalent circle diameter of less than 20 nm disappear in a short
time in high-temperature heating upon high heat input welding, thereby little contribute
to the inhibition of austenite grain coarsening, and do not require special control.

[0032] Titanium nitride particles are energetically unstable with a decreasing size thereof.
Specifically, titanium nitride particles more readily disappear upon HAZ high-temperature
heating with a smaller (decreasing) size as compared to the average size of all titanium
nitride particles. For this reason, particles that contribute to austenite grain coarsening
inhibition are substantially present in an increasing number with an increasing number
of titanium nitride particles having a larger size than the average size, or having
a size smaller than, but relatively near to, the average size.
[0033] The present inventors have found herein as follows. When a size-number histogram
of titanium nitride particles is plotted, the size and number of the particles are
preferably controlled so that the difference between the average size and a size in
which the largest number of titanium nitride particles is recorded becomes small.
This increases the number of the substantially contributive titanium nitride particles
and achieves highly effective inhibition of austenite grain coarsening.
[0034] More specifically, the control may be performed that the difference between values
df and da becomes small. The df is defined as follows. The titanium nitride particles
having an equivalent circle diameter of 20 nm or more are classified into ranges of
equivalent circle diameter from 20 nm up to 500 nm every 5 nm in an increasing order,
in which particles in each of the ranges have an equivalent circle diameter of (di-5)
to less than di, where di is 25, 30, 35,...500, and the di in a range having a largest
number of titanium nitride particles present in the range is defined as the df. The
da represents the average equivalent circle diameter of the titanium nitride particles
having an equivalent circle diameter of 20 nm to less than 500 nm. This control increases
the number of substantially contributive titanium nitride particles and achieves highly
effective inhibition of austenite grain coarsening.
[0035] The average equivalent circle diameter of titanium nitride particles was calculated
in the following manner. Specifically, a sample was subjected to transmission electron
microscopic (TEM) observation under conditions mentioned below in experimental examples.
The areas of individual titanium nitride particles in the observation view field were
measured by image analysis, from which equivalent circle diameters of the individual
titanium nitride particles were calculated Of the particles, titanium nitride particles
having an equivalent circle diameter of 20 nm to less than 500 nm were selected, and
the arithmetic mean of the equivalent circle diameters of the selected particles was
determined
[0036] Specifically, if the value specified by the formula: |da-df|/da is greater than 0.35,
titanium nitride particles, even if present in a large number, may fail to sufficiently
inhibit austenite grain coarsening and fail to provide satisfactory HAZ toughness
upon high heat input.
Production Method
[0037] The steel plate according to the present invention meets the above-mentioned conditions.
Specifically, the steel plate contains oxide particles including constituent elements
excluding oxygen in contents, in mass percent, meeting conditions: 2% < Ti < 40%,
5% < Al < 30%, 5% < Ca < 40%, 5% < REM < 50%, 2% < Zr < 30%, and 1.0 ≤ REM/Zr. Of
the oxide particles, oxide particles having an equivalent circle diameter of less
than 2 µm are present in a number density of 300 or more per square millimeter; and
oxide particles having an equivalent circle diameter of 2 µm or more are present in
a number density of 100 or less per square millimeter. Of titanium nitride particles
contained in the steel plate, titanium nitride particles having an equivalent circle
diameter of 1 µm or more are present in a number density of 7 or less per square millimeter,
and titanium nitride particles having an equivalent circle diameter of 20 nm or more
are present in a number density of 1.0x 10
6 or more per square millimeter. In addition, the steel plate meets the conditions
as specified by the relational expression of |da-df|/da ≤ 0.35. The steel plate is
preferably produced under production conditions as follows.
[0038] The preferred production conditions are as follows. In ingot-making, the dissolved
oxygen content in the molten steel is controlled to the range of 0.002% to 0.01% (in
mass percent) by deoxidation typically using Mn and Si. Thereafter Al, Ti, (REM, Zr),
and Ca are added in the specified order in such a controlled manner that a time t1
from the REM or Zr addition to the Ca addition be 5 minutes or longer. In addition,
a cooling time t2 in the temperature range of 1500°C to 1450°C upon casting may be
set within 300 seconds, and a cooling time t3 in the temperature range of 1300°C to
1200°C upon casting may be set within 680 seconds. In a preferred embodiment, the
mass ratio [REM]/[Zr] of the REM content [REM] to the Zr content [Zr] may be controlled
to 1.8 or more, and the time t1 may be controlled to 10 minutes or longer. This may
provide more an appropriate oxide particle form and reduce the amount of coarsely
formed titanium nitride particles in the surface of the oxide particles to give still
better HAZ toughness. Next, why the production conditions are specified will be described
in detail below. As used herein the term "(REM, Zr)" refers to that REM and Zr may
be added simultaneously or non-simultaneously in any order.
[0039] Initially, the dissolved oxygen content in the molten steel is controlled to the
range of 0.002% to 0.01% by deoxidation typically using Mn and Si.
[0040] The dissolved oxygen, if present in a content less than 0.002%, may fail to provide
a necessary amount of oxide particles having such an appropriate chemical composition
as to induce intragranular ferrite formation. The dissolved oxygen, if present in
a content greater than 0.01%, may cause the formation of a larger amount of coarse
oxide particles having an equivalent circle diameter of 2 µm or more to cause the
steel plate to have inferior HAZ toughness.
[0041] Secondary, the time t1 from the addition of REM or Zr to the addition of Ca is controlled
to 5 minutes or longer.
[0042] The oxides specified in the present invention effectively promote intragranular ferrite
formation and hardly function as nucleation sites for coarse titanium nitride particles.
In particular to allow the REM/Zr ratio (in mass percent) in the oxides to be 1.0
or more, an oxide formation reaction of REM or Zr preferably proceeds sufficiently
before the addition of Ca that acts as a strong deoxidizing element. Specifically,
the time t1 from the addition of REM or Zr to the addition of Ca is preferably controlled
to 5 minutes or longer. This can give oxide particles that are present in a predetermined
number density and meet the condition: REM/Zr ≥ 1.0. If the time t1 from the addition
of REM or Zr to the addition of Ca is shorter than 5 minutes, oxide particles meeting
the condition: REM/Zr ≥ 1.0 may be formed insufficiently. In a preferred embodiment,
the mass ratio [REM]/[Zr] of the REM content [REM] to the Zr content [Zr] is controlled
to 1.8 or more, and the time t1 is controlled to 10 minutes or longer. This can give
oxide particles that are present in a predetermined number density and meet the condition:
REM/Zr ≥ 1.5.
[0043] The elements Al, Ti, (REM, Zr), and Ca are added in the specified order in ingot
making. This is because these elements, if added in a order other than the specified
order, may fail to ensure a sufficient number of oxide particles having such an appropriate
chemical composition as to act as nucleation sites of intragranular ferrite. In particular,
Ca is a strong deoxidizing element and has extremely strong deoxidation power and,
if added prior to Ti and Al, may significantly reduce the amount of oxygen to be combined
with Ti and Al.
[0044] The cooling time t2 in the temperature range of 1500°C to 1450°C upon casting is
controlled within 300 seconds.
[0045] If the cooling time t2 in the temperature range of 1500°C to 1450°C upon casting
is longer than 300 seconds, coarse oxide particles may be increased, or coarse titanium
nitride particles may be formed due to component segregation upon solidification,
to cause the steel plate to have inferior HAZ toughness.
[0046] The cooling time t3 in the temperature range of 1300°C to 1200°C upon casting is
controlled within 680 seconds.
[0047] If the cooling time t3 in the temperature range of 1300°C to 1200°C upon casting
is longer than 680 seconds, the relational expression of |da-df|/da ≤ 0.35 may not
be satisfied. This is probably because as follows.
[0048] Titanium nitride particles formed upon casting are classified into A, B, and C as
follows. The titanium nitride particles A are those formed in the molten steel. The
titanium nitride particles B are those formed in a solidification segregation portion
of the solidified steel. The titanium nitride particles are those formed in a non-solidification-segregation
portion of the solidified steel. The titanium nitride particles A, B, and C are formed
in the specified order and have sizes (particle diameters) in decreasing order (A
> B > C). In contrast, the titanium nitride particles A, B, and C are present in increasing
order of number (A < B < C). Most of titanium nitride particles having sizes corresponding
to the df are the titanium nitride particles C. The titanium nitride particles A are
present in a smaller number as compared with the titanium nitride particles B and
C and little affect the average equivalent circle diameter da of titanium nitride
particles. It is therefore considered that, to control the value specified by
[0049] I |da-df|/da within a predetermined range, the formation of the titanium nitride
particles B and C is preferably controlled. Assume that the cooling time t3 in the
temperature range of 1300°C to 1200°C upon casting is longer than 680 seconds. In
this case, the titanium nitride particles B grow prior to the formation of the titanium
nitride particles C and may cause the specific titanium nitride particles to have
a larger average equivalent circle diameter da, to probably cause the value specified
by |da-df|/da to be greater than 0.35.
Chemical Compositions
[0050] Next, the chemical compositions of the steel plate according to the present invention
will be described. Assume that the steel plate according to the present invention
includes individual chemical compositions (elements) in contents out of appropriate
ranges. In this case, the base metal (steel plate) may fail to have properties and
the HAZ at good levels even when the steel plate includes oxide particles in the appropriate
dispersion state as described above. Accordingly, the steel plate according to the
present invention includes chemical compositions in contents within ranges as described
below. The contents of elements constituting oxides, such as Al, Ca, and Ti, among
the chemical compositions, are contents as including part of the elements constituting
the oxides. The contents (%) of the chemical compositions are all in mass percent.
C of 0.03% to 0.12%
[0051] Carbon (C) element is essential for ensuring the strength of the steel plate. Carbon,
if present in a content less than 0.03%, may fail to provide a necessary strength.
In contrast, carbon, if present in an excessively high content, may cause the formation
of a large amount of hard martensite-austenite constituent (MA) to cause the base
metal to have inferior toughness. To prevent this, the carbon content may be controlled
to 0.12% or less. Of the carbon content, the lower limit is preferably 0.04%, and
the upper limit is preferably 0.10%.
Si of 0.10% to 0.25%
[0052] Silicon (Si) element allows titanium (Ti) to have higher activity and may be added
as appropriate to provide the predetermined titanium nitride particle form. Si, if
added in an amount of less than 0.10%, may fail to allow the titanium nitride particles
having an equivalent circle diameter of 20 nm or more to be present in a number density
of 1.0x 10
6 per square millimeter or more. Si, if added in an amount of greater than 0.25%, may
readily cause the formation of coarse titanium nitride particles and the formation
of a hard MA phase, to fail to provide a predetermined HAZ toughness. Of the Si content,
the lower limit is preferably 0.12% and more preferably 0.14%, and the upper limit
is preferably 0.22% and more preferably 0.20%.
Mn of 1.0% to 2.0%
[0053] Manganese (Mn) element is useful in ensuring the strength of the steel plate. To
allow the element to exhibit such effects effectively, Mn is preferably present in
a content of 1.0% or more. However, Mn, if present in an excessively high content
of greater than 2.0%, may cause the HAZ to have an excessively high strength and to
have inferior toughness. To prevent this, the Mn content is preferably 2.0% or less.
Of the Mn content, the lower limit is preferably 1.4%, and the upper limit is preferably
1.8%.
P of 0.03% or less (excluding 0%)
[0054] Phosphorus (P) element is an impurity element that readily causes grain boundary
fracture and adversely affects the toughness. To prevent this, the phosphorus content
is preferably minimized. From the viewpoint of ensuring the HAZ toughness, the phosphorus
content is controlled to 0.03% or less, and preferably 0.02% or less. However, it
is difficult to industrially control the phosphorus content in the steel to 0%.
S of 0.015% or less (excluding 0%)
[0055] Sulfur (S) element forms manganese sulfide at the prior austenite grain boundary
in the HAZ and causes the steel plate to have inferior HAZ toughness. To prevent this,
the sulfur content is preferably minimized. From the viewpoint of ensuring the HAZ
toughness, the sulfur content is controlled to 0.015% or less, and preferably 0.010%
or less. However, it is difficult to industrially control the sulfur content in the
steel to 0%.
Al of 0.004% to 0.05%
[0056] Aluminum (Al) element forms oxides that act as nucleation sites for intragranular
ferrite. Al, if present in a content of less than 0.004%, may fail to provide the
predetermined oxide form and fail to sufficiently promote intragranular transformation
to cause the steel plate to have inferior HAZ toughness. In contrast, Al, if present
in an excessively high content, may cause the formation of coarse oxide particles
to cause the steel plate to have inferior HAZ toughness. To prevent this, the Al content
may be controlled to 0.05% or less. Of the Al content, the lower limit is preferably
0.007%, and the upper limit is preferably 0.04%.
Ti of 0.010% to 0.050%
[0057] Titanium (Ti) element forms titanium nitride and, when added prior to REM, Zr, and
Ca, enables fine dispersion of oxides that effectively promote intragranular ferrite
formation. To provide the predetermined titanium nitride arid oxide forms, Ti may
be contained in a content of 0.010% or more. However, Ti, if present in an excessively
high content, may cause the formation of a larger amount of coarse titanium nitride
particles to cause the steel plate to have inferior HAZ toughness. To prevent this,
the Ti content may be controlled to 0.050% or less. Of the Ti content, the lower limit
is preferably 0.012%, and the upper limit is preferably 0.035% and more preferably
0.025%.
REM of 0.0003% to 0.02% and Zr of 0.0003% to 0.02%
[0058] Rare-earth elements (REM) and zirconium (Zr) element, when added after the addition
of Ti but before the addition of Ca, form oxides that are effective in intragranular
ferrite formation. These oxides, when compositively precipitated with titanium nitride,
more suitably act as intragranular ferrite formation sites. The elements exhibit these
effects increasingly with increasing contents. To allow the elements to exhibit the
effects effectively, REM and Zr may be present each in a content of 0.0003% or more.
However, these elements, if present in an excessively high content, may cause the
oxides to be coarsened to cause the steel plate to have inferior HAZ toughness. To
prevent this, the contents of REM and Zr may be each controlled to 0.02% or less.
Of the contents of these elements, the lower limit is more preferably 0.0005%, and
the upper limit is more preferably 0.015%.
Ca of 0.0005% to 0.010%
[0059] Calcium (Ca) element, when added 5 minutes or longer after the addition of REM and
Zr (in any order), forms oxides that are effective in intragranular ferrite formation
and inhibit the formation of coarse titanium nitride particles. To allow the element
to exhibit such effects effectively, Ca may be contained in a content of 0.0005% or
more. However, Ca, if present in an excessively high content, may form coarse oxide
particles to cause the steel plate to have inferior HAZ toughness. To prevent this,
the Ca content may be controlled to 0.010% or less. Of the Ca content, the lower limit
is preferably 0.0008%, and the upper limit is preferably 0.008%.
N of 0.002% to 0.010%
[0060] Nitrogen (N) element, when forming fine titanium nitride particles, is useful in
ensuring the HAZ toughness. Nitrogen, if present in a content of 0.002% or more, may
provide the desired titanium nitride particles. However, nitrogen, if present in an
excessively high content, may promote the formation of coarse titanium nitride particles.
To prevent this, the nitrogen content may be controlled to 0.010% or less. Of the
nitrogen content, the lower limit is preferably 0.003%, and the upper limit is preferably
0.008%.
[0061] The above-mentioned elements are essential elements specified in the present invention,
with the remainder being iron and inevitable impurities. As inevitable impurities,
Sn, As, Pb, and other elements may be contained, where the elements are brought into
the steel under circumstances of raw materials, facility materials, and production
facilities. It is also effective to actively add any of elements as follows. This
may allow the steel plate to have further better property or properties depending
on the type of the chemical composition (element) to be added.
[0062] In a preferred embodiment, at least one element selected from the group consisting
of Ni of 0.05% to 1.50%, Cu of 0.05% to 1.50%, Cr of 0.05% to 1.50%, and Mo of 0.05%
to 1.50% may be added.
[0063] Nickel (Ni), copper (Cu), Chromium (Cr), and molybdenum (Mo) elements are each effective
in allowing the steel plate to have a higher strength. These elements exhibit increasing
effects with increasing contents. To allow the elements to exhibit such effects effectively,
the elements are preferably contained each in a content of 0.05% or more. However,
the elements, if present in an excessively high content, may cause the steel plate
to have an excessively high strength and to have inferior HAZ toughness. To prevent
this, the contents of the elements are each preferably controlled to 1.50% or less.
Of each of the contents of the elements, the lower limit is more preferably 0.10%,
and the upper limit is more preferably 1.20%.
[0064] In a preferred embodiment, at least one of Nb of 0.002% to 0.10% and V of 0.002%
to 0.10% may be added.
[0065] Niobium (Nb) and vanadium (V) elements precipitate as carbonitrides, inhibit the
coarsening of austenite grains, and are effective in allowing the base metal to have
good toughness. These elements exhibit increasing effects with increasing contents.
To allow the elements to exhibit such effects effectively, the elements are preferably
contained each in a content of 0.002% or more. However, the elements, if contained
in excessively high contents, may cause the coarsening of the HAZ microstructure to
cause the steel plate to have inferior HAZ toughness. To prevent this, the contents
of the elements are each preferably controlled to 0.10% or less. Of each of the contents
of the elements, the lower limit is more preferably 0.005%, and the upper limit is
more preferably 0.08%.
In a preferred embodiment, B of 0.0005% to 0.0050% may be added
[0066] Boron (B) element inhibits the formation of coarse grain boundary ferrite and effectively
allows the steel plate to have better HAZ toughness. The element exhibits an increasing
effect as above with an increasing content thereof. To allow the element to exhibit
such effects effectively, the element is preferably contained in a content of 0.0005%
or more. The boron content is more preferably 0.0010% or more, and furthermore preferably
0.0015% or more. However, boron, if present in an excessively high content, may promote
the formation of a coarse bainite packet at prior austenite grain boundaries to cause
the steel plate to have inferior HAZ toughness contrarily. Of the boron content, the
upper limit is preferably 0.0045%, more preferably 0.0040%, and furthermore preferably
0.0035%.
[0067] As is described in the description of chemical compositions, it is effective for
the steel plate to contain at least one element selected from the group consisting
of Ni, Cu, Cr, and Mo. In this case, the contents (in mass percent) of these elements
preferably meet the condition: [Ni]+[Cu]+[Cr]+[Mo] < 2.5%, where [Ni], [Cu], [Cr],
and [Mo] are contents (in mass percent) respectively of Ni, Cu, Cr, and Mo.
[0068] Coarse titanium nitride particles are formed in a liquid phase in a solidification
stage of the molten steel, where Ti and N are enriched in the liquid phase due to
solidification segregation. The elements, when present in a total content ([Ni]+[Cu]+[Cr]+[Mo])
of greater than 2.5%, may cause the solidification temperature to be lowered. This
may cause the liquid phase to remain even cooled down to a low temperature. At such
low temperatures, the driving force for the formation of coarse titanium nitride particles
becomes large to cause the formation of a larger amount of the coarse titanium nitride
particles.

[0069] The value specified by |da-df|/da is a parameter that relates to the number of titanium
nitride particles contributing to austenite grain coarsening inhibition upon HAZ high-temperature
heating. If the value is greater than 0.35, the austenite grains are not sufficiently
inhibited from coarsening and fail to provide predetermined HAZ toughness. The upper
limit of the value is preferably 0.30 and more preferably 0.25.
[0070] The present invention relates to steel plates. In general, the term "steel plate"
refers to a steel sheet having a thickness of 3.0 mm or more as defined in Japanese
Industrial Standards (JIS). In contrast, the steel plate according to the present
invention has been invented as targeting the welding of steel plates having a thickness
of 50 mm or more. In this connection, the target steel sheets herein may be considered
to be steel sheets (steel plates) having a thickness of 50 mm or more. It should be
noted, however, that these are merely preferred embodiments and are never intended
to exclude the application of the present invention to steel plates having a thickness
of less than 50 mm. Examples
[0071] The present invention will be illustrated in further detail with reference to several
examples (experimental examples) below. It should be noted, however, that the examples
are by no means intended to limit the scope of the present invention; that various
changes and modifications can naturally be made therein without deviating from the
spirit and scope of the present invention as described herein; and all such changes
and modifications should be considered to be within the scope of the present invention.
[0072] In examples (experimental examples) in the present invention, steel plates were produced
in the following manner. Initially, molten steels having chemical compositions given
in Tables 1 and 2 were prepared using a vacuum induction furnace (VIF: 150 kg). The
molten steels were cast to give slabs (150 mm by 250 mm in section). The slabs were
subjected to hot rolling and yielded hot-rolled plates having a thickness of 80 mm.
The hot rolling was performed under conditions as follows. Prior to rolling, heating
was performed at 1100°C for 3 hours. Then the hot rolling was performed at a finish
rolling temperature of 780°C or higher, an average cooling rate down to 450°C of 6°C/s,
and a cooling stop temperature of 450°C.
[0073] Upon production of the hot-rolled plates (steel plates), conditions as follows were
controlled, as indicated in Tables 3 and 4. The controlled conditions are the dissolved
oxygen content [Of] (in mass percent) in the molten steel before the addition of Al
(Ti); the order of the additions of Al, Ti, REM, Zr, and Ca; the time t1 from the
addition of REM or Zr to the addition of Ca; the mass ratio [REM]/[Zr] of the REM
content [REM] to the Zr content [Zr], where this ratio is indicated as "REM/Zr" in
the tables; the cooling time t2 in the temperature range of 1500°C to 1450°C upon
casting; and the cooling time t3 in the temperature range of 1300°C to 1200°C upon
casting.
[0074] REM as in Tables 1 and 2 was added in the form of a misch metal containing, in mass
percent, about 50% of Ce and about 25% of La. The symbol "-" in Tables 1 and 2 refers
to that an element in question was not added
[0075] In Tables 3 and 4, the order of the additions of Al, Ti, REM, Zr, and Ca is indicated
as "○" when the elements were added in the specified order of Al, Ti, (REM, Zr), and
Ca; and is indicated as "×" when the elements were added in any order excluding the
specified order.
[Table 1]
| No. |
C |
Si |
Mn |
P |
S |
Al |
Ti |
REM |
Zr |
Ca |
N |
Ni |
Cu |
Cr |
Mo |
Nb |
V |
B |
| 1 |
0.05 |
0.19 |
1.56 |
0.006 |
0.002 |
0.010 |
0.018 |
0.0020 |
0.0018 |
0.0018 |
0.0062 |
- |
- |
- |
- |
- |
- |
- |
| 2 |
0.04 |
0.16 |
1.51 |
0.009 |
0.002 |
0.012 |
0.017 |
0.0022 |
0.0019 |
0.0021 |
0.0072 |
- |
- |
- |
- |
- |
- |
- |
| 3 |
0.08 |
0.15 |
1.72 |
0.007 |
0.003 |
0.008 |
0.015 |
0.0023 |
0.0010 |
0.0017 |
0.0048 |
- |
- |
- |
- |
- |
- |
- |
| 4 |
0.06 |
0.19 |
1.46 |
0.007 |
0.002 |
0.025 |
0.020 |
0.0019 |
0.0022 |
0.0016 |
0.0042 |
- |
- |
- |
- |
- |
- |
- |
| 5 |
0.07 |
0.16 |
1.58 |
0.010 |
0.002 |
0.007 |
0.019 |
0.0018 |
0.0017 |
0.0012 |
0.0056 |
0.25 |
- |
- |
- |
- |
- |
- |
| 6 |
0.10 |
0.15 |
1.51 |
0.007 |
0.002 |
0.008 |
0.020 |
0.0021 |
0.0018 |
0.0009 |
0.0055 |
- |
0.35 |
- |
- |
- |
- |
- |
| 7 |
0.05 |
0.21 |
1.13 |
0.026 |
0.001 |
0.011 |
0.021 |
0.0020 |
0.0016 |
0.0015 |
0.0069 |
- |
- |
0.62 |
- |
- |
- |
- |
| 8 |
0.11 |
0.16 |
1.46 |
0.006 |
0.001 |
0.007 |
0.017 |
0.0022 |
0.0018 |
0.0038 |
0.0075 |
- |
- |
- |
0.19 |
- |
- |
- |
| 9 |
0.08 |
0.17 |
1.62 |
0.018 |
0.002 |
0.007 |
0.023 |
0.0018 |
0.0014 |
0.0032 |
0.0038 |
0.45 |
- |
0.25 |
- |
- |
- |
- |
| 10 |
0.04 |
0.22 |
1.69 |
0.005 |
0.002 |
0.008 |
0.016 |
0.0017 |
0.0018 |
0.0020 |
0.0046 |
- |
- |
- |
- |
0.016 |
- |
- |
| 11 |
0.05 |
0.14 |
1.50 |
0.006 |
0.002 |
0.031 |
0.011 |
0.0007 |
0.0006 |
0.0016 |
0.0049 |
- |
- |
- |
- |
- |
0.028 |
- |
| 12 |
0.09 |
0.16 |
1.77 |
0.008 |
0.001 |
0.009 |
0.013 |
0.0015 |
0.0011 |
0.0023 |
0.0046 |
- |
- |
- |
- |
- |
- |
0.0019 |
| 13 |
0.08 |
0.18 |
1.70 |
0.007 |
0.003 |
0.010 |
0.015 |
0.0030 |
0.0013 |
0.0069 |
0.0055 |
0.23 |
- |
0.68 |
- |
- |
- |
- |
| 14 |
0.05 |
0.17 |
1.63 |
0.004 |
0.013 |
0.012 |
0.026 |
0.0024 |
0.0023 |
0.0018 |
0.0047 |
1.07 |
0.86 |
1.24 |
- |
- |
- |
- |
| 15 |
0.09 |
0.15 |
1.51 |
0.008 |
0.002 |
0.016 |
0.020 |
0.0026 |
0.0024 |
0.0023 |
0.0042 |
0.99 |
0.25 |
0.71 |
0.38 |
- |
- |
- |
| 16 |
0.05 |
0.15 |
1.53 |
0.007 |
0.002 |
0.014 |
0.020 |
0.0068 |
0.0019 |
0.0039 |
0.0059 |
1.25 |
0.10 |
- |
- |
0.012 |
- |
- |
| 17 |
0.08 |
0.12 |
1.49 |
0.009 |
0.002 |
0.008 |
0.022 |
0.0038 |
0.0025 |
0.0009 |
0.0079 |
0.55 |
0.35 |
- |
0.24 |
- |
- |
0.0014 |
| 18 |
0.04 |
0.15 |
1.56 |
0.004 |
0.002 |
0.015 |
0.020 |
0.0019 |
0.0010 |
0.0017 |
0.0042 |
1.15 |
0.45 |
0.68 |
0.34 |
- |
- |
|
| 19 |
0.03 |
0.16 |
1.92 |
0.007 |
0.005 |
0.017 |
0.017 |
0.0024 |
0.0018 |
0.0027 |
0.0063 |
- |
- |
- |
- |
- |
- |
- |
| 20 |
0.10 |
0.17 |
1.88 |
0.007 |
0.002 |
0.008 |
0.033 |
0.0015 |
0.0012 |
0.0016 |
0.0049 |
- |
- |
0.07 |
- |
0.088 |
- |
- |
| 21 |
0.06 |
0.19 |
1.46 |
0.004 |
0.008 |
0.010 |
0.027 |
0.0042 |
0.0009 |
0.0017 |
0.0085 |
0.25 |
0.16 |
- |
1.25 |
- |
- |
- |
| 22 |
0.10 |
0.12 |
1.50 |
0.011 |
0.003 |
0.005 |
0.012 |
0.0030 |
0.0020 |
0.0014 |
0.0062 |
- |
- |
0.39 |
0.06 |
- |
0.035 |
0.0007 |
| 23 |
0.05 |
0.11 |
1.52 |
0.009 |
0.001 |
0.014 |
0.036 |
0.0022 |
0.0010 |
0.0015 |
0.0074 |
- |
- |
- |
- |
0.063 |
|
|
| 24 |
0.04 |
0.24 |
1.59 |
0.008 |
0.001 |
0.023 |
0.014 |
0.0031 |
0.0020 |
0.0019 |
0.0063 |
- |
0.15 |
- |
- |
|
0.088 |
- |
| 25 |
0.06 |
0.14 |
1.60 |
0.009 |
0.002 |
0.044 |
0.016 |
0.0004 |
0.0011 |
0.0016 |
0.0051 |
0.38 |
0.22 |
- |
- |
0.009 |
- |
0.0029 |
| 26 |
0.05 |
0.17 |
1.53 |
0.008 |
0.001 |
0.030 |
0.047 |
0.0036 |
0.0018 |
0.0017 |
0.0048 |
- |
- |
- |
- |
- |
0.063 |
|
| 27 |
0.09 |
0.12 |
1.57 |
0.007 |
0.001 |
0.028 |
0.017 |
0.0008 |
0.0008 |
0.0023 |
0.0070 |
0.56 |
0.81 |
- |
- |
- |
|
0.0042 |
| 28 |
0.05 |
0.14 |
1.58 |
0.007 |
0.001 |
0.010 |
0.016 |
0.0016 |
0.0021 |
0.0031 |
0.0048 |
0.41 |
0.26 |
- |
- |
0.009 |
- |
0.0025 |
| 29 |
0.06 |
0.21 |
1.58 |
0.007 |
0.009 |
0.020 |
0.016 |
0.0032 |
0.0024 |
0.0016 |
0.0042 |
- |
- |
- |
0.79 |
- |
- |
- |
| 30 |
0.05 |
0.18 |
1.72 |
0.017 |
0.001 |
0.016 |
0.019 |
0.0155 |
0.0153 |
0.0024 |
0.0059 |
0.46 |
0.23 |
0.89 |
- |
- |
- |
0.0021 |
| 31 |
0.04 |
0.17 |
1.41 |
0.006 |
0.002 |
0.011 |
0.030 |
0.0013 |
0.0004 |
0.0019 |
0.0062 |
- |
- |
- |
- |
0.016 |
0.025 |
- |
| 32 |
0.10 |
0.15 |
1.63 |
0.007 |
0.002 |
0.007 |
0.026 |
0.0028 |
0.0015 |
0.0008 |
0.0026 |
0.07 |
0.07 |
- |
- |
- |
- |
0.0033 |
| 33 |
0.06 |
0.20 |
1.62 |
0.006 |
0.003 |
0.013 |
0.019 |
0.0033 |
0.0029 |
0.0007 |
0.0061 |
- |
- |
- |
- |
0.004 |
0.004 |
- |
| 34 |
0.09 |
0.14 |
1.49 |
0.007 |
0.002 |
0.012 |
0.020 |
0.0020 |
0.0012 |
0.0084 |
0.0050 |
- |
- |
- |
- |
|
0.009 |
0.0025 |
| 35 |
0.05 |
0.13 |
1.72 |
0.007 |
0.001 |
0.011 |
0.025 |
0.0024 |
0.0013 |
0.0022 |
0.0041 |
0.72 |
1.25 |
0.26 |
- |
- |
|
|
[Table 2]
| No. |
C |
Si |
Mn |
P |
S |
Al |
Ti |
REM |
Zr |
Ca |
N |
Ni |
Cu |
Cr |
Mo |
Nb |
V |
B |
| 36 |
0.09 |
0.15 |
1.46 |
0.006 |
0.002 |
0.008 |
0.016 |
0.0018 |
0.0020 |
0.0020 |
0.0051 |
- |
- |
- |
- |
- |
- |
- |
| 37 |
0.08 |
0.14 |
1.53 |
0.007 |
0.001 |
0.008 |
0.015 |
0.0024 |
0.0021 |
0.0019 |
0.0039 |
- |
- |
- |
- |
- |
- |
- |
| 38 |
0.07 |
0.13 |
1.75 |
0.008 |
0.002 |
0.009 |
0.013 |
0.0013 |
0.0011 |
0.0020 |
0.0066 |
- |
- |
- |
- |
- |
- |
- |
| 39 |
0.08 |
0.21 |
1.42 |
0.009 |
0.002 |
0.012 |
0.019 |
0.0017 |
0.0015 |
0.0021 |
0.0057 |
- |
- |
- |
- |
- |
- |
- |
| 40 |
0.05 |
0.19 |
1.63 |
0.006 |
0.001 |
0.018 |
0.017 |
0.0029 |
0.0025 |
0.0015 |
0.0071 |
- |
- |
- |
- |
- |
- |
- |
| 41 |
0.04 |
0.17 |
1.60 |
0.007 |
0.003 |
0.016 |
0.016 |
0.0018 |
0.0020 |
0.0013 |
0.0079 |
- |
- |
- |
- |
- |
- |
- |
| 42 |
0.04 |
0.09 |
1.71 |
0.006 |
0.002 |
0.020 |
0.023 |
0.0015 |
0.0013 |
0.0010 |
0.0070 |
- |
- |
- |
- |
- |
- |
- |
| 43 |
0.07 |
0.26 |
1.73 |
0.007 |
0.001 |
0.016 |
0.021 |
0.0013 |
0.0013 |
0.0012 |
0.0066 |
- |
- |
- |
- |
- |
- |
- |
| 44 |
0.09 |
0.21 |
1.56 |
0.032 |
0.002 |
0.009 |
0.018 |
0.0016 |
0.0020 |
0.0018 |
0.0105 |
- |
- |
- |
- |
- |
- |
- |
| 45 |
0.05 |
0.17 |
1.55 |
0.009 |
0.002 |
0.003 |
0.020 |
0.0019 |
0.0021 |
0.0017 |
0.0069 |
- |
- |
- |
- |
- |
- |
- |
| 46 |
0.06 |
0.19 |
1.48 |
0.006 |
0.007 |
0.051 |
0.051 |
0.0015 |
0.0017 |
0.0015 |
0.0058 |
- |
- |
1.58 |
- |
- |
- |
- |
| 47 |
0.07 |
0.16 |
1.52 |
0.005 |
0.009 |
0.026 |
0.009 |
0.0012 |
0.0019 |
0.0016 |
0.0047 |
0.51 |
1.52 |
- |
- |
- |
- |
- |
| 48 |
0.05 |
0.15 |
1.62 |
0.004 |
0.003 |
0.008 |
0.015 |
0.0002 |
0.0018 |
0.0019 |
0.0070 |
1.54 |
- |
- |
- |
- |
- |
- |
| 49 |
0.04 |
0.18 |
1.64 |
0.007 |
0.016 |
0.009 |
0.032 |
0.0211 |
0.0017 |
0.0020 |
0.0060 |
- |
- |
- |
1.57 |
- |
- |
- |
| 50 |
0.06 |
0.17 |
1.58 |
0.007 |
0.002 |
0.010 |
0.034 |
0.0018 |
0.0001 |
0.0021 |
0.0040 |
- |
- |
- |
- |
0.105 |
- |
- |
| 51 |
0.04 |
0.19 |
2.03 |
0.009 |
0.001 |
0.007 |
0.026 |
0.0021 |
0.0206 |
0.0010 |
0.0040 |
- |
- |
0.25 |
- |
- |
- |
- |
| 52 |
0.13 |
0.14 |
1.75 |
0.006 |
0.001 |
0.015 |
0.018 |
0.0020 |
0.0020 |
0.0004 |
0.0046 |
- |
- |
- |
- |
- |
- |
- |
| 53 |
0.05 |
0.13 |
1.42 |
0.007 |
0.001 |
0.017 |
0.017 |
0.0027 |
0.0017 |
0.0024 |
0.0018 |
- |
- |
- |
- |
- |
- |
- |
| 54 |
0.05 |
0.17 |
1.59 |
0.007 |
0.006 |
0.019 |
0.016 |
0.0020 |
0.0019 |
0.0105 |
0.0046 |
- |
- |
- |
- |
- |
0.106 |
- |
| 55 |
0.05 |
0.18 |
1.48 |
0.007j |
0.005 |
0.028 |
0.023 |
0.0045 |
0.0011 |
0.0037 |
0.0071 |
- |
- |
- |
- |
- |
- |
0.0053 |
[Table 3]
| No. |
[Of] mass percent |
Order of addition |
t1 (min) |
REM/Zr |
t2(s) |
t3(s) |
| 1 |
0.0030 |
○ |
7 |
1.6 |
271 |
530 |
| 2 |
0.0041 |
○ |
5 |
1.8 |
255 |
530 |
| 3 |
0.0035 |
○ |
15 |
3.0 |
263 |
530 |
| 4 |
0.0036 |
○ |
12 |
1.5 |
256 |
530 |
| 5 |
0.0048 |
○ |
7 |
1.4 |
259 |
480 |
| 6 |
0.0042 |
○ |
12 |
1.7 |
271 |
660 |
| 7 |
0.0030 |
○ |
10 |
1.9 |
268 |
530 |
| 8 |
0.0026 |
○ |
25 |
1.8 |
292 |
530 |
| 9 |
0.0051 |
○ |
10 |
2.0 |
245 |
500 |
| 10 |
0.0051 |
○ |
15 |
1.6 |
268 |
530 |
| 11 |
0.0063 |
○ |
5 |
1.5 |
281 |
500 |
| 12 |
0.0038 |
○ |
20 |
2.0 |
277 |
530 |
| 13 |
0.0052 |
○ |
35 |
2.8 |
270 |
530 |
| 14 |
0.0026 |
○ |
12 |
1.3 |
245 |
480 |
| 15 |
0.0035 |
○ |
20 |
2.0 |
213 |
530 |
| 16 |
0.0077 |
○ |
7 |
6.7 |
239 |
530 |
| 17 |
0.0039 |
○ |
5 |
2.0 |
188 |
600 |
| 18 |
0.0031 |
○ |
12 |
3.0 |
251 |
530 |
| 19 |
0.0022 |
○ |
5 |
2.4 |
246 |
530 |
| 20 |
0.0022 |
○ |
25 |
2.7 |
191 |
530 |
| 21 |
0.0027 |
○ |
18 |
12.0 |
210 |
500 |
| 22 |
0.0043 |
○ |
7 |
2.0 |
253 |
660 |
| 23 |
0.0086 |
○ |
20 |
2.5 |
225 |
600 |
| 24 |
0.0053 |
○ |
12 |
2.8 |
270 |
530 |
| 25 |
0.0040 |
○ |
65 |
1.0 |
268 |
530 |
| 26 |
0.0027 |
○ |
55 |
4.8 |
259 |
530 |
| 27 |
0.0030 |
○ |
12 |
2.5 |
260 |
500 |
| 28 |
0.0027 |
○ |
7 |
1.6 |
245 |
500 |
| 29 |
0.0039 |
○ |
20 |
2.0 |
211 |
530 |
| 30 |
0.0091 |
○ |
25 |
1.9 |
278 |
530 |
| 31 |
0.0025 |
○ |
7 |
5.0 |
288 |
500 |
| 32 |
0.0053 |
○ |
12 |
3.0 |
206 |
530 |
| 33 |
0.0038 |
○ |
60 |
2.0 |
225 |
500 |
| 34 |
0.0031 |
○ |
40 |
3.0 |
271 |
530 |
| 35 |
0.0066 |
○ |
35 |
3.7 |
284 |
530 |
[Table 4]
| No. |
[Of] mass percent |
Order of addition |
t1(min) |
REM/Zr |
t2(s) |
t3(s) |
| 36 |
0.0059 |
○ |
3 |
1.6 |
270 |
530 |
| 37 |
0.0041 |
× |
15 |
1.7 |
271 |
530 |
| 38 |
0.0107 |
○ |
7 |
1.2 |
231 |
530 |
| 39 |
0.0018 |
○ |
12 |
1.9 |
286 |
500 |
| 40 |
0.0033 |
○ |
45 |
1.7 |
275 |
720 |
| 41 |
0.0032 |
○ |
50 |
1.2 |
310 |
480 |
| 42 |
0.0030 |
○ |
5 |
2.0 |
270 |
530 |
| 43 |
0.0024 |
○ |
7 |
1.9 |
288 |
530 |
| 44 |
0.0041 |
○ |
20 |
1.4 |
265 |
600 |
| 45 |
0.0051 |
○ |
18 |
1.2 |
276 |
530 |
| 46 |
0.0023 |
○ |
5 |
1.8 |
261 |
530 |
| 47 |
0.0046 |
○ |
12 |
1.0 |
250 |
530 |
| 48 |
0.0033 |
○ |
20 |
0.3 |
292 |
660 |
| 49 |
0.0028 |
○ |
15 |
20.0 |
261 |
500 |
| 50 |
0.0034 |
○ |
5 |
15.0 |
259 |
530 |
| 51 |
0.0025 |
○ |
20 |
0.2 |
280 |
500 |
| 52 |
0.0039 |
○ |
25 |
1.5 |
274 |
530 |
| 53 |
0.0039 |
○ |
12 |
2.2 |
288 |
530 |
| 54 |
0.0042 |
○ |
25 |
1.5 |
249 |
600 |
| 55 |
0.0042 |
○ |
12 |
7.3 |
240 |
530 |
[0076] The hot-rolled plates (steel plates) produced under the conditions as above were
each subjected to measurements of number densities N1, NA, N2, N3, and N4, the value
|da-df|/da, and HAZ toughness by measurement methods below. The number density N1
refers to the number density of oxide particles having an equivalent circle diameter
of less than 2 pm, containing Ti, Al, Ca, REM, and Zr in contents within the predetermined
ranges, and having a ratio [REM]/[Zr] of equal to or greater than 1.0. The number
density NA refers to the number density of oxide particles having an equivalent circle
diameter of less than 2 µm, containing Ti, Al, Ca, REM, and Zr in contents within
the predetermined ranges, and having a ratio [REM]/[Zr] of equal to or greater than
1.5. The number densityN2 refers to the number density of oxide particles having an
equivalent circle diameter of 2 µm or more. The number density N3 refers to the number
density of titanium nitride particles having an equivalent circle diameter of 1 µm
or more. The number density N4 refers to the number density of titanium nitride particles
having an equivalent circle diameter of 20 nm or more. The measurement results are
indicated in Tables 5 and 6.
Number Density Measurement of Oxide Particles Having Equivalent Circle Diameter of
Less Than 2 µm
[0077] Test specimens were cut out from the steel plates in a position at a depth of one-fourth
the thickness from the surface so that the axis of the test specimen passed through
the position at a depth of one-fourth the thickness. The test specimens were observed
in a cross section in parallel with the rolling direction and thickness direction
using the field emission scanning electron microscope SUPRA35 (trade name) supplied
by Carl Zeiss AG. The field emission scanning electron microscope is hereinafter also
simply referred to as FE-SEM. The observation was performed at 5000-fold magnification
in an observation area of 0.048 mm
2. The areas of individual oxide particles in the observation view field were measured
by image analysis, and based on which the equivalent circle diameters of the oxide
particles were calculated. Whether the oxide particles had chemical compositions meeting
the conditions was determined using an energy dispersive X-ray spectrometer (EDX)).
The chemical composition measurement using the EDX was performed at an acceleration
voltage of 15 kV for a measurement time of 100 seconds. The numbers (N1, NA) of oxide
particles having an equivalent circle diameter of less than 2 µm were determined each
as a number density per square millimeter. However, oxide particles having an equivalent
circle diameter of 0.2 µm or less did not have sufficient reliability in EDX analysis
and were excluded from the analysis.
Number Density Measurement of Oxide Particles Having Equivalent Circle Diameter of
2 µm or More
[0078] Test specimens were cut out from the steel plates in a position at a depth of one-fourth
the thickness from the surface so that the axis of the test specimen passed through
the position at a depth of one-fourth the thickness. The test specimens were observed
in a cross section in parallel with the rolling direction and thickness direction
using the FE-SEM The observation was performed at 1000-fold magnification in an observation
view field of 0.06 mm
2 at 20 points. The areas of individual oxide particles in the observation view field
were measured by image analysis, and based on which the equivalent circle diameters
of the oxide particles were calculated. Whether the oxide particles had chemical compositions
meeting the conditions was determined using an energy dispersive X-ray spectrometer
(EDX)). The chemical composition measurement using the EDX was performed at an acceleration
voltage of 15 kV for a measurement time of 100 seconds. The number (N2) of oxide particles
having an equivalent circle diameter of 2 µm or more was determined as a number density
per square millimeter.
Number Density Measurement of Titanium Nitride Particles Having Equivalent Circle
Diameter of 1 µm or More
[0079] Test specimens were cut out from the steel plates in a position at a depth of one-fourth
the thickness from the surface so that the axis of the test specimen passed through
the position at a depth of one-fourth the thickness. The test specimens were observed
in a cross section in parallel with the rolling direction and thickness direction,
and images of 20 view fields in the cross section were taken using an optical microscope
at 200-fold magnification. The number of coarse titanium nitride particles was counted
and converted into a number density (N3) per square millimeter. The measured images
have an area of 0.148 mm
2 per view field and an area of 2.96 mm
2 per test specimen. Titanium nitride particles were identified based on shape and
color. Vivid orange, angular inclusions were considered as titanium nitride particles.
The equivalent circle diameters of the titanium nitride particles were calculated
using an analysis software. A coarse titanium nitride particle often forms with an
oxide as a nucleation site. In this case, the oxide in the titanium nitride was excluded
from the object for the measurement of equivalent circle diameter.
Number Density Measurement of Titanium Nitride Particles Having Equivalent Circle
Diameter of 20 nm or More, and Calculation of |da-df| /da
[0080] Specimens were cut out from the steel plates in a position at a depth of one-fourth
the thickness. The cross sections of the specimens in parallel with the rolling direction
and thickness direction were treated to give replica TEM test specimens. The replica
TEM test specimens were observed with a transmission electron microscope (TEM) at
15000-fold magnification in 4 view fields each having an area of 6.84 µm by 8.05 µm,
based on which particles containing Ti and N were identified using an energy dispersive
X-ray fluorescence spectrometer (EDX) and treated as titanium-containing nitrides.
The areas of titanium-containing nitrides in the view fields were measured by image
analysis and converted into equivalent circle diameters. The number of titanium-containing
nitride particles having an equivalent circle diameter of 20 nm or more was determined
and converted into a value per square millimeter to give the number density (N4).
Based on the resulting data, df and da were determined as follows. The titanium nitride
particles having an equivalent circle diameter of 20 nm or more were classified into
ranges of equivalent circle diameter from 20 nm up to 500 nm every 5 nm in an increasing
order, in which particles in each of the ranges had an equivalent circle diameter
of (di-5) to less than di, where di is 25, 30, 35,...500, and the di in a range having
a largest number of titanium nitride particles present in the range was defined as
the df. The da was defined as the average equivalent circle diameter of titanium nitride
particles having an equivalent circle diameter of 20 nm to less than 500 nm. Thus,
the value | da-df | /da was calculated
HAZ Toughness Evaluation
[0081] Specimens for weld joint was sampled from the steel plates, processed to have a V
groove, and subjected to electrogas arc welding with a heat input of 50 kJ/mm. Each
three Charpy impact test specimens (V-notched test specimens prescribed in JIS Z 2242)
were sampled from the specimens, where the test specimens had notches in a heat affected
zone (HAZ) adjacent to the weld line (bond) in a position at a depth of one-fourth
the thickness from the surface of the steel plate. The Charpy impact test specimens
were subjected to Charpy impact tests at -40°C to measure absorbed energy (vE
-40). Of the measured absorbed energy, the average and minimum were determined A specimen
having an average vE
-40 of greater than 180 J and a minimum vE
-40 of greater than 120 J was evaluated as having excellent HAZ toughness.
[0082] Independently, three test specimens were prepared and subjected to Charpy impact
tests under the conditions as mentioned above, except for performing electrogas arc
welding with a heat input of 60 kJ/mm to measure absorbed energy (vE
-40) of the three specimens, and the average of which was determined Based on the measured
data, a specimen having an average vE
-40 of greater than 120 J was evaluated as having excellent HAZ toughness; and a specimen
having an average vE
-40 of greater than 150 J was evaluated as having particularly excellent HAZ toughness.
[Table 5]
| No. |
N1 (per mm2) |
NA (per mm2) |
N2 (per mm2) |
N3 (per mm2) |
N4 (x106 per mm2) |
|da—df|/da |
HAZ toughness vE-40 (J) |
| 50kJ/mm |
60kJ/mm |
| Average |
Minimum |
Average |
| 1 |
313 |
208 |
12 |
4.1 |
1.3 |
0.10 |
187 |
153 |
131 |
| 2 |
375 |
271 |
18 |
3.4 |
1.5 |
0.11 |
194 |
176 |
135 |
| 3 |
500 |
354 |
13 |
1.0 |
1.7 |
0.12 |
235 |
207 |
160 |
| 4 |
417 |
271 |
19 |
3.4 |
1.2 |
0.10 |
208 |
171 |
145 |
| 5 |
333 |
208 |
22 |
4.4 |
1.3 |
0.07 |
185 |
129 |
129 |
| 6 |
396 |
292 |
20 |
3.0 |
1.3 |
0.34 |
190 |
141 |
128 |
| 7 |
479 |
313 |
15 |
1.7 |
2.2 |
0.16 |
208 |
186 |
154 |
| 8 |
458 |
333 |
16 |
2.0 |
2.1 |
0.23 |
188 |
156 |
151 |
| 9 |
542 |
375 |
26 |
0.7 |
1.6 |
0.08 |
237 |
221 |
165 |
| 10 |
438 |
292 |
25 |
3.4 |
1.2 |
0.12 |
190 |
146 |
132 |
| 11 |
354 |
188 |
33 |
4.7 |
1.0 |
0.12 |
184 |
128 |
122 |
| 12 |
500 |
354 |
15 |
1.4 |
1.5 |
0.10 |
228 |
200 |
153 |
| 13 |
563 |
396 |
27 |
1.7 |
1.6 |
0.11 |
235 |
215 |
162 |
| 14 |
396 |
229 |
8 |
6.4 |
1.2 |
0.09 |
182 |
135 |
123 |
| 15 |
500 |
333 |
32 |
1.0 |
1.5 |
0.08 |
225 |
218 |
156 |
| 16 |
396 |
271 |
63 |
3.4 |
1.5 |
0.12 |
198 |
166 |
132 |
| 17 |
375 |
292 |
15 |
3.0 |
1.4 |
0.07 |
208 |
200 |
148 |
| 18 |
521 |
375 |
8 |
5.7 |
1.1 |
0.12 |
187 |
172 |
152 |
| 19 |
313 |
271 |
7 |
3.4 |
1.5 |
0.13 |
190 |
172 |
136 |
| 20 |
521 |
313 |
6 |
1.7 |
1.9 |
0.08 |
194 |
144 |
151 |
| 21 |
667 |
500 |
13 |
4.4 |
1.5 |
0.11 |
182 |
125 |
153 |
| 22 |
333 |
250 |
10 |
3.4 |
1.4 |
0.32 |
191 |
166 |
143 |
| 23 |
625 |
417 |
83 |
4.4 |
1.1 |
0.23 |
205 |
190 |
158 |
| 24 |
563 |
396 |
32 |
4.7 |
1.3 |
0.10 |
210 |
190 |
152 |
| 25 |
375 |
250 |
93 |
4.1 |
1.4 |
0.12 |
182 |
125 |
123 |
| 26 |
542 |
396 |
63 |
4.7 |
2.6 |
0.10 |
213 |
176 |
159 |
| 27 |
479 |
333 |
15 |
0.7 |
2.0 |
0.13 |
214 |
199 |
152 |
| 28 |
333 |
208 |
11 |
4.4 |
1.3 |
0.09 |
196 |
166 |
130 |
| 29 |
521 |
333 |
10 |
1.0 |
1.7 |
0.10 |
231 |
206 |
159 |
| 30 |
792 |
417 |
97 |
1.4 |
1.9 |
0.11 |
201 |
125 |
151 |
| 31 |
354 |
271 |
15 |
3.0 |
1.5 |
0.18 |
215 |
186 |
142 |
| 32 |
521 |
375 |
17 |
0.3 |
1.4 |
0.16 |
203 |
171 |
155 |
| 33 |
375 |
333 |
18 |
2.7 |
1.8 |
0.12 |
229 |
207 |
159 |
| 34 |
521 |
375 |
87 |
1.4 |
1.8 |
0.10 |
208 |
133 |
152 |
| 35 |
583 |
438 |
43 |
2.4 |
1.6 |
0.18 |
210 |
181 |
156 |
[Table 6]
| No. |
N1 (per mm2) |
NA (per mm2) |
N2 (per mm2) |
N3 (per mm2) |
N4 (x106 per mm2) |
|da-df|/da |
HAZ toughness vE-40 (J) |
| 50kJ/mm |
60kJ/mm |
| Average |
Minimum |
Average |
| 36 |
292 |
208 |
28 |
4.1 |
1.4 |
0.15 |
177 |
140 |
115 |
| 37 |
271 |
188 |
15 |
4.4 |
1.3 |
0.14 |
176 |
139 |
103 |
| 38 |
354 |
208 |
111 |
4.7 |
1.3 |
0.13 |
184 |
105 |
128 |
| 39 |
292 |
208 |
7 |
3.4 |
1.5 |
0.10 |
176 |
151 |
115 |
| 40 |
417 |
292 |
18 B |
3.7 |
1.1 |
0.36 |
175 |
145 |
113 |
| 41 |
375 |
250 |
103 |
7.1 |
0.8 |
0.22 |
166 |
103 |
91 |
| 42 |
375 |
250 |
17 |
0.7 |
0.9 |
0.15 |
175 |
161 |
134 |
| 43 |
396 |
250 |
13 |
7.4 |
1.1 |
0.21 |
170 |
115 |
126 |
| 44 |
396 |
292 |
19 |
7.1 |
2.1 |
0.17 |
128 |
61 |
88 |
| 45 |
292 |
208 |
23 |
5.1 |
1.1 |
0.12 |
170 |
116 |
115 |
| 46 |
333 |
208 |
127 |
7.8 |
0.8 |
0.12 |
106 |
38 |
67 |
| 47 |
250 |
208 |
44 |
3.4 |
0.9 |
0.15 |
165 |
110 |
93 |
| 48 |
271 |
125 |
12 |
4.4 |
1.3 |
0.30 |
160 |
113 |
82 |
| 49 |
729 |
604 |
117 |
2.4 |
2.3 |
0.10 |
131 |
64 |
90 |
| 50 |
292 |
167 |
13 |
3.4 |
1.5 |
0.13 |
158 |
125 |
97 |
| 51 |
313 |
167 |
123 |
3.0 |
1.5 |
0.28 |
125 |
51 |
65 |
| 52 |
271 |
229 |
13 |
7.1 |
1.4 |
0.11 |
151 |
82 |
101 |
| 53 |
479 |
333 |
20 |
0.0 |
0.9 |
0.31 |
177 |
165 |
124 |
| 54 |
438 |
292 |
117 |
3.7 |
1.3 |
0.12 |
145 |
88 |
98 |
| 55 |
625 |
563 |
29 |
1.4 |
2.3 |
0.12 |
170 |
134 |
115 |
[0083] The data demonstrate that the steel plates of Nos.1 to 35 are examples meeting conditions
specified in the present invention and were appropriately controlled typically in
chemical compositions and the dispersion of oxide particles and titanium nitride particles.
These steel plates had excellent HAZ toughness (average and minimum) with a heat input
of 50 kJ/mm and excellent HAZ toughness (average) with a heat input of 60 kJ/mm. Specifically,
the steel plates of Nos.1 to 35 can be considered as steel plates having excellent
heat affected zone toughness.
[0084] Of the steel plates, those meeting the conditions specified in the second embodiment
had an average vE
-40 of greater than 150 J and were evaluated as steel plates having particularly excellent
heat affected zone toughness.
[0085] In contrast, the steel plates of Nos. 36 to 55 are comparative examples not meeting
at least one of the conditions specified in the present invention. The data demonstrate
that these steel plates failed to meet the criterion in either one of the HAZ toughness
(average and minimum) with a heat input of 50 kJ/mm and the HAZ toughness (average)
with a heat input of 60 kJ/mm.
[0086] While the present invention has been described in detail with reference to specific
embodiments, it is apparent to those skilled in the art that various changes and modifications
can be made therein without deviating from the spirit and scope of the present invention.
Industrial Applicability
[0088] The steel plate according to the present invention has excellent toughness in a heat
affected zone after high heat input and is useful in welded structures such as bridges,
high-rise buildings, ships, and line pipes.