Technical Field
[0001] The present invention relates to a steel material for a high-strength line pipe with
high fracture toughness in hydrogen in a high-pressure hydrogen gas environment of
1 MPa or more, a method for producing the steel material, a steel pipe for a high-strength
line pipe, and a method for producing the steel pipe, suitable for applications, such
as a line pipe for transporting hydrogen gas.
Background Art
[0002] As an existing energy infrastructure, there is a line pipe for transporting crude
oil, natural gas, or the like. Such a steel structure is used in an atmosphere containing
hydrogen sulfide, and the occurrence of hydrogen embrittlement, such as hydrogen-induced
cracking (HIC) or sulfide stress corrosion cracking (SSCC), has become a safety problem,
and suppression thereof has been required. To prevent the occurrence of hydrogen embrittlement,
such as hydrogen-induced cracking or sulfide stress corrosion cracking, various measures
have been taken, such as reducing amount of MnS as an origin of a crack in a steel
material, suppressing accumulation of carbonitride or oxide of Ti or Nb, or suppressing
segregation of hardened phase of center segregation. From the perspective of suppressing
the occurrence of origin of a crack by improving the corrosion resistance of a steel
material, addition of Sn or Sb to the steel material has been proposed (for example,
Patent Literature 1 and Patent Literature 2).
[0003] In recent years, utilization of hydrogen has been promoted as a clean energy source
for the purpose of building a decarbonizing society. Thus, for the purpose of transporting
a large amount of hydrogen gas, construction of a hydrogen gas transportation network
that pressure-feeds natural gas mixed with a certain percentage of hydrogen or hydrogen
gas as an alternative through a natural gas line pipe has been studied. The transport
pressure in such a pipeline operation is assumed to be a high pressure in the range
of 1 to 40 MPa, and a line pipe is exposed to a high-pressure hydrogen gas environment.
A steel material used in such an environment needs to have hydrogen resistance required
in a hydrogen gas environment in addition to characteristics required in an existing
sour environment, that is, suppression of occurrence of corrosion on an inner surface
of a steel pipe and reduction of accumulation of hydrogen in the material.
[0004] Austenite stainless steel, such as SUS 316L, which exhibits fracture toughness in
hydrogen, is used for a steel structure used in a high-pressure hydrogen gas environment.
However, such a steel material is expensive, has low strength, and when designed to
be able to withstand a high hydrogen pressure, has a large wall thickness, resulting
in a very expensive line pipe and, therefore, not suitable for laying a pipeline.
Thus, there has been a demand for a steel material that can withstand a high-pressure
hydrogen gas environment at a lower cost for use in a hydrogen line pipe.
[0005] To solve the above problems, for example, Patent Literature 3 proposes an austenitic
steel material with a high Mn content. According to the technique described in Patent
Literature 3, it is possible to provide a steel material at lower cost than austenite
stainless steel, but the steel material is austenitic and is therefore higher in cost
than low-alloy steel. Furthermore, suppression of pitting corrosion as an origin of
a hydrogen-induced, such as HIC resistance or SSCC resistance, is not considered.
[0006] Furthermore, in a pipeline, the operation is repeatedly started and shut down, applying
repeated stress to a line pipe. Thus, when designing a steel structure, such as a
pipeline, it is essential to consider fatigue fracture. The breaking point of fatigue
fracture of a steel structure used in a high-pressure hydrogen gas environment corresponds
to the critical crack length calculated from the operating conditions of the pipeline
and the hydrogen-induced crack growth threshold K
IH corresponding to the fracture toughness value of the steel material in hydrogen gas.
From the perspective of extending the life and improving the safety of a structure
for hydrogen, increasing the K
IH of a steel material is considered to be an effective guide.
[0007] A hydrogen pipeline is assumed to use a line pipe with a weld, that is, a welded
metal portion, and a heat-affected zone [HAZ]. Patent Literature 4 proposes a method
for producing a steel material with high K
IH but does not refer to the characteristics of a weld. In general, a weld is more susceptible
to characteristic degradation due to hydrogen than a base material. Thus, it is important
to improve the K
IH also for a weld.
[0008] To increase the K
IH of a steel material, for example, it is better to decrease upper bainite containing
a coarse carbide.
Citation List
Patent Literature
Summary of Invention
Technical Problem
[0011] The present invention has been made to solve these known problems and aims to provide
a steel material for a high-strength line pipe with high fracture toughness in hydrogen
in a high-pressure hydrogen gas environment, a method for producing the steel material,
a steel pipe for a high-strength line pipe, and a method for producing the steel pipe,
suitable for a steel structure used in a high-pressure hydrogen gas environment, such
as a line pipe for 100% hydrogen gas or a natural gas containing hydrogen at a hydrogen
partial pressure of 1 MPa or more (natural gas is a gas containing hydrocarbons, such
as methane and ethane, as main components). The high-pressure hydrogen gas environment
is assumed to be a high-pressure hydrogen gas of 1 MPa or more or an environment containing
0.2% or more of hydrogen gas.
[0012] The phrase "high fracture toughness in hydrogen in a high-pressure hydrogen gas environment",
as used herein, refers to a hydrogen-induced crack growth threshold K
IH of 80 MPa·m
1/2 or more, as determined by a fracture toughness test at room temperature (20°C ± 10°C)
in both environments of hydrogen gas with a pressure of 1 MPa or more and a natural
gas (the main components are hydrocarbons, such as methane and ethane) mixed atmosphere
containing hydrogen at a hydrogen partial pressure of 1 MPa or more. The fracture
toughness value refers to a value determined by a fracture toughness test according
to ASTM E399, ASTM E1820, and ASTM E1681. The natural gas containing hydrogen with
a hydrogen partial pressure of 1 MPa or more, for example, has a hydrogen concentration
of 30% or less by volume and a pressure of the entire gas of 30 MPa or less.
[0013] The term "steel material", as used herein, includes a steel sheet, a steel plate,
a seamless steel pipe, an electric-resistance-welded steel pipe, a shaped steel, a
steel bar, and the like.
Solution to Problem
[0014] For the purpose of suppressing hydrogen absorption into a steel material, which is
a fundamental factor of hydrogen embrittlement, the present inventors have made technical
studies on conditions to be satisfied by the steel material to produce a steel material
for a high-strength line pipe and a steel pipe for a high-strength line pipe with
high fracture toughness in hydrogen in a high-pressure hydrogen gas environment. As
a result, it has been found that the hydrogen-induced crack growth threshold K
IH of a steel material or a steel pipe is improved in a metallic microstructure in which
the number of inclusions with an aspect ratio of 2.0 or more and a length of 10 µm
or more is 15 pieces/100 mm
2 or less and the bainite in the range from a surface of the steel material or the
steel pipe to the middle of the sheet thickness has a maximum grain size of 25 µm
or less. It has also been found that the hydrogen-induced crack growth threshold K
IH of a steel material is further improved when an area fraction of retained austenite
is 0% to 3% and an area fraction of bainite in the range from a surface of the steel
material or a steel pipe to the middle of the sheet thickness is 90% or more. To realize
such a steel microstructure, it is necessary to strictly control the rolling conditions
in a hot rolling step and the cooling conditions after rolling, and these conditions
have been successfully discovered. The present invention is based on these findings.
In the present invention, the term "high strength" refers to a tensile strength of
520 MPa or more.
[0015] Thus, the gist of the present invention is as follows:
- [1] A steel material for a high-strength line pipe with high fracture toughness in
hydrogen, the steel material including:
a chemical composition containing:
on a mass percent basis,
C: 0.02% to 0.15%,
Si: 0.01% to 2.0%,
Mn: 0.5% to 1.5%,
P: 0.0001% to 0.015%,
S: 0.0002% to 0.0015%,
Al: 0.005% to 0.15%,
O: 0.01% or less,
N: 0.010% or less,
Nb: 0.10% or less, and
H: 0.02 ppm or less, and
optionally at least one selected from
Ca: 0% to 0.005%,
Ni: 0% to 2.0%,
Ti: 0% to 0.1%,
Cu: 0% to 1.0%,
Cr: 0% to 1.0%,
Mo: 0% to 0.60%,
W: 0% to 1.0%,
V: 0% to 0.10%,
Zr: 0% to 0.050%,
Mg: 0% to 0.01%,
REM: 0% to 0.01%,
B: 0% to 0.0020%,
Ta: 0% to 0.2%,
Hf: 0% to 0.2%,
Re: 0% to 0.005%,
Sn: 0% to 0.3%, and
Sb: 0% to 0.3%,
the remainder being Fe and an incidental impurity element,
a metallic microstructure containing bainite and 15 pieces/100 mm2 or less of inclusions having an aspect ratio of 2.0 or more and a length of 10 µm
or more, the bainite in a range from a surface to a middle of a thickness of the steel
material having a maximum grain size of 25 µm or less,
tensile strength of 520 MPa or more, and
a hydrogen-induced crack growth threshold KIH in a high-pressure hydrogen gas environment of 1 MPa or more of 80 MPa·m1/2 or more.
- [2] The steel material for a high-strength line pipe with high fracture toughness
in hydrogen according to [1], wherein the chemical composition contains, on a mass
percent basis,
Ca: 0.0001% to 0.005%,
Ni: 0.01% to 2.0%,
Ti: 0.005% to 0.1%,
Cu: 0.01% to 1.0%,
Cr: 0.01% to 1.0%,
Mo: 0.01% to 0.60%,
W: 0.01% to 1.0%,
V: 0.01% to 0.10%,
Zr: 0.0001% to 0.050%,
Mg: 0.0001% to 0.01%,
REM: 0.0001% to 0.01%,
B: 0.0001% to 0.0020%,
Ta: 0.0001% to 0.2%,
Hf: 0.0001% to 0.2%,
Re: 0.0001% to 0.005%,
Sn: 0.0001% to 0.3%, and
Sb: 0.0001% to 0.3%.
- [3] The steel material for a high-strength line pipe with high fracture toughness
in hydrogen according to [1] or [2], wherein an area fraction of retained austenite
is 0% to 3% by area, and an area fraction of the bainite in the range from the surface
to the middle of the thickness of the steel material is 90% or more.
- [4] A method for producing a steel material for a high-strength line pipe with high
fracture toughness in hydrogen, the method including:
a heating step of heating a cast steel having the chemical composition according to
[1] or [2] at 1000°C to 1250°C;
a hot rolling step of rolling the cast steel heated in the heating step under conditions
in which a total rolling reduction in a recrystallization temperature range is 35%
or more and 55% or less, a rolling reduction in a final rolling pass in the recrystallization
temperature range is 10% or more, a rolling reduction in a final rolling pass at (recrystallization
temperature - 80°C) or more is 15% or more, and a finish rolling temperature is an
Ar3 transformation point or higher in terms of a temperature at a surface of a steel
sheet; and
a controlled cooling step of cooling a hot-rolled steel sheet produced in the hot
rolling step under conditions in which a cooling start temperature is the Ar3 transformation point or higher in terms of a temperature at the surface of the hot-rolled
steel sheet, a cooling start time difference between a front end and a rear end of
the hot-rolled steel sheet is 50 seconds or less, an average cooling rate from 750°C
to 550°C ranges from 15°C/s to 50°C/s in terms of a temperature at a middle of a thickness
of the steel sheet, and a cooling stop temperature ranges from 250°C to 650°C.
- [5] A steel pipe for a high-strength line pipe with high fracture toughness in hydrogen,
the steel pipe including:
a chemical composition containing:
on a mass percent basis,
C: 0.02% to 0.15%,
Si: 0.01% to 2.0%,
Mn: 0.5% to 1.5%,
P: 0.0001% to 0.015%,
S: 0.0002% to 0.0015%,
Al: 0.005% to 0.15%,
O: 0.01% or less,
N: 0.010% or less,
Nb: 0.10% or less, and
H: 0.02 ppm or less, and
optionally at least one selected from
Ca: 0% to 0.005%,
Ni: 0% to 2.0%,
Ti: 0% to 0.1%,
Cu: 0% to 1.0%,
Cr: 0% to 1.0%,
Mo: 0% to 0.60%,
W: 0% to 1.0%,
V: 0% to 0.10%,
Zr: 0% to 0.050%,
Mg: 0% to 0.01%,
REM: 0% to 0.01%,
B: 0% to 0.0020%,
Ta: 0% to 0.2%,
Hf: 0% to 0.2%,
Re: 0% to 0.005%,
Sn: 0% to 0.3%, and
Sb: 0% to 0.3%,
the remainder being Fe and an incidental impurity element,
a metallic microstructure containing bainite and 15 pieces/100 mm2 or less of inclusions having an aspect ratio of 2.0 or more and a length of 10 µm
or more, the bainite in a range from an inner surface to a middle of a thickness of
the steel pipe having a maximum grain size of 25 µm or less,
tensile strength of 520 MPa or more, and
a hydrogen-induced crack growth threshold KIH in a high-pressure hydrogen gas environment of 1 MPa or more of 80 MPa·m1/2 or more.
- [6] The steel pipe for a high-strength line pipe with high fracture toughness in hydrogen
according to [5], wherein the chemical composition contains, on a mass percent basis,
Ca: 0.0001% to 0.005%,
Ni: 0.01% to 2.0%,
Ti: 0.005% to 0.1%,
Cu: 0.01% to 1.0%,
Cr: 0.01% to 1.0%,
Mo: 0.01% to 0.60%,
W: 0.01% to 1.0%,
V: 0.01% to 0.10%,
Zr: 0.0001% to 0.050%,
Mg: 0.0001% to 0.01%,
REM: 0.0001% to 0.01%,
B: 0.0001% to 0.0020%,
Ta: 0.0001% to 0.2%,
Hf: 0.0001% to 0.2%,
Re: 0.0001% to 0.005%,
Sn: 0.0001% to 0.3%, and
Sb: 0.0001% to 0.3%.
- [7] The steel pipe for a high-strength line pipe with high fracture toughness in hydrogen
according to [5] or [6], wherein an area fraction of retained austenite is 0% to 3%,
and an area fraction of the bainite in the range from the inner surface to the middle
of the thickness of the steel pipe is 90% or more.
- [8] A method for producing a steel pipe for a high-strength line pipe with high fracture
toughness in hydrogen, the method including:
a heating step of heating a cast steel having the chemical composition according to
[5] or [6] at 1000°C to 1250°C;
a hot rolling step of rolling the cast steel heated in the heating step under conditions
in which a total rolling reduction in a recrystallization temperature range is 35%
or more and 55% or less, a rolling reduction in a final rolling pass in the recrystallization
temperature range is 10% or more, a rolling reduction in a final rolling pass at (recrystallization
temperature - 80°C) or more is 15% or more, and a finish rolling temperature is an
Ar3 transformation point or higher in terms of a temperature of a surface of a steel
sheet;
a controlled cooling step of cooling a hot-rolled steel sheet produced in the hot
rolling step under conditions in which a cooling start temperature is the Ar3 transformation point or higher in terms of a temperature at a surface of the hot-rolled
steel sheet, a cooling start time difference between a front end and a rear end of
the hot-rolled steel sheet is 50 seconds or less, an average cooling rate from 750°C
to 550°C ranges from 15°C/s to 50°C/s in terms of a temperature at a middle of a thickness
of the steel sheet, and a cooling stop temperature ranges from 250°C to 650°C; and
any one of a pipe production step of bending the hot-rolled steel sheet and butt-welding
both end portions thereof after the controlled cooling step and a pipe production
step of forming the hot-rolled steel sheet into a cylindrical shape by cold roll forming
and subjecting both circumferential end portions of the cylindrical shape to butt
electric resistance welding after the controlled cooling step.
Advantageous Effects of Invention
[0016] The present invention can easily and simply produce a steel material with considerably
improved fracture toughness in hydrogen in a high-pressure hydrogen gas environment
and exhibits industrially significant effects. The present invention also has the
effects of significantly improving the hydrogen absorption resistance of a steel structure,
such as a high-pressure hydrogen gas line pipe, and greatly contributing to the improvement
of the safety of the steel structure.
Description of Embodiments
[0017] Next, a method for implementing the present invention is more specifically described.
[0018] A steel material is more specifically described as a first embodiment, a UOE steel
pipe as an example of a steel pipe according to the present invention is more specifically
described as a second embodiment, and an electric-resistance-welded steel pipe as
an example of a steel pipe according to the present invention is more specifically
described as a third embodiment.
First Embodiment
[Chemical Composition]
[0019] The reasons for limiting base material components in a steel material according to
the present invention are described below. Unless otherwise specified, the unit "%"
in the following description refers to "% by mass".
C: 0.02% to 0.15%
[0020] C effectively contributes to the improvement of strength, but the strength cannot
be sufficient at a C content of less than 0.02%, so that the C content is 0.02% or
more. Preferably, the C content is 0.03% or more. More preferably, the C content is
0.035% or more. Still more preferably, the C content is 0.04% or more. On the other
hand, more than 0.15% results in low weldability. Thus, the C content is limited to
0.15% or less. Preferably, the C content is 0.10% or less. More than 0.08% may result
in a decrease in SSCC resistance and HIC resistance due to an increase in the hardness
of a surface layer portion or a center segregation zone during controlled cooling.
Furthermore, toughness also deteriorates. Thus, the C content is more preferably 0.08%
or less. Still more preferably, the C content is 0.06% or less.
Si: 0.01% to 2.0%
[0021] Si is contained for deoxidization, but the deoxidation effect is not sufficient at
a content of less than 0.01%, so that the Si content is 0.01% or more. The Si content
is preferably 0.02% or more. More preferably, the Si content is 0.05% or more. Still
more preferably, the Si content is 0.08% or more. The effect is observed up to 2.0%,
and the Si content is therefore 2.0% or less. The Si content is preferably 1.8% or
less, more preferably 1.5% or less. The Si content is still more preferably 1.0% or
less. However, more than 0.5% sometimes results in lower toughness or weldability,
and the Si content is therefore most preferably 0.5% or less.
Mn: 0.5% to 1.5%
[0022] Mn effectively contributes to the improvement of strength and toughness, but the
effect of containing Mn is insufficient at a content of less than 0.5%, so that the
Mn content is 0.5% or more. The Mn content is preferably 0.6% or more, more preferably
0.8% or more. Still more preferably, the Mn content is 1.0% or more. On the other
hand, more than 1.5% results in lower SSCC resistance and HIC resistance due to an
increase in the hardness of a surface layer portion or a center segregation zone during
controlled cooling. Furthermore, weldability also deteriorates. Thus, the Mn content
is limited to 1.5% or less. Preferably, the Mn content is 1.4% or less. The Mn content
is more preferably 1.3% or less, still more preferably 1.2% or less.
P: 0.0001% to 0.015%
[0023] P is an incidental impurity element, reduces weldability, and reduces the HIC resistance
due to an increase in the hardness of a center segregation zone. This tendency becomes
remarkable at more than 0.015%, and the P content is therefore limited to 0.015% or
less. The P content is preferably 0.012% or less, more preferably 0.010% or less.
Still more preferably, the P content is 0.008% or less. Although a lower P content
is better, from the perspective of refining costs, the P content is 0.0001% or more.
S: 0.0002% to 0.0015%
[0024] S is an incidental impurity element, forms a MnS inclusion in steel, and reduces
the HIC resistance, so that a lower S content is preferred, but 0.0015% or less is
allowable. Thus, the S content is 0.0015% or less. The S content is preferably 0.0010%
or less, more preferably 0.0008% or less. Although a lower S content is better, from
the perspective of refining costs, the S content is 0.0002% or more.
Al: 0.005% to 0.15%
[0025] Al is added as a deoxidizing agent, and the effect of containing Al is insufficient
at less than 0.005%, so that the Al content is 0.005% or more. On the other hand,
more than 0.15% results in steel with lower cleanliness and toughness, so that the
Al content is 0.15% or less. The Al content is preferably 0.12% or less, more preferably
0.10% or less. Still more preferably, the Al content is 0.08% or less.
O: 0.01% or less
[0026] O causes the formation of an oxide inclusion, and the O content is therefore preferably
as small as possible. This influence does not become a problem at an O content of
0.01% or less, and the O content is therefore 0.01% or less. The O content is preferably
0.0080% or less. More preferably, the O content is less than 0.0030%. The lower limit
may be, but is not limited to, 0.0005% or more.
N: 0.010% or less
[0027] N effectively contributes to the improvement of the strength, but a content of more
than 0.010% results in an increase in the hardness during controlled cooling and lower
toughness. Thus, the N content is 0.010% or less. The N content is preferably 0.008%
or less, more preferably 0.006% or less, still more preferably 0.004% or less. However,
sufficient strength cannot be ensured at less than 0.00001%, and an excessive decrease
increases the steelmaking cost. Thus, the content is preferably 0.00001% or more.
More preferably, the N content is 0.002% or more.
Nb: 0.10% or less
[0028] Nb is an element effective in increasing the strength and toughness of a steel material.
The effects of containing Nb are insufficient at a content of less than 0.001%, and
0.001% or more is therefore preferred. On the other hand, more than 0.10% results
in a weld with lower toughness, and the Nb content is therefore 0.10% or less. The
Nb content is preferably 0.095% or less. The Nb content is more preferably 0.090%
or less, still more preferably 0.085% or less. The Nb content is most preferably 0.080%
or less.
H: 0.02 ppm or less
[0029] H may be introduced into a steel material in various steps during production, and
a large amount of H introduced may increase the risk of cracking after solidification
and significantly reduce the K
IH. These effects do not cause a problem at 0.02 ppm or less, and the H content is therefore
0.02 ppm or less. The H content is preferably 0.015 ppm or less, more preferably 0.008
ppm or less. The H content is still more preferably 0.005 ppm or less, most preferably
less than 0.002 ppm. The lower limit is preferably, but not limited to, 0.0008 ppm
or more from the perspective of production cost. The H content is more preferably
0.001 ppm or more. The amount of hydrogen is the amount of residual hydrogen after
forming of a steel material, a steel pipe, UOE, or the like.
[0030] The chemical composition in the present disclosure may optionally contain at least
one selected from Ca, Ni, Ti, Cu, Cr, Mo, W, V, Zr, Mg, REM, B, Ta, Hf, Re, Sn, and
Sb in the following range.
Ca: 0% to 0.005%
[0031] Ca is an element effective in improving the HIC resistance by the shape control of
a sulfide inclusion, and when Ca is contained, the Ca content may be 0% or more, but
the effect of addition is insufficient at less than 0.0001%. Thus, when Ca is contained,
the Ca content is 0.0001% or more, more preferably 0.0005% or more. On the other hand,
at more than 0.005%, not only the effect is saturated but also the HIC resistance
decreases due to a decrease in the cleanliness of steel, so that when Ca is contained
the Ca content is limited to 0.005% or less. The Ca content is preferably 0.004% or
less. The Ca content is more preferably 0.002% or less, still more preferably 0.0008%
or less.
Ni: 0% to 2.0%
[0032] Ni is an element effective in improving the toughness and increasing the strength,
and when Ni is contained, the Ni content may be 0% or more, but to achieve these effects,
it is preferable to contain 0.01% or more. The Ni content is more preferably 0.1%
or more. On the other hand, to reduce the cost, when Ni is contained, the Ni content
is 2.0% or less. The Ni content is preferably 1.8% or less. The Ni content is more
preferably 1.4% or less, still more preferably 0.8% or less.
Ti: 0% to 0.1%
[0033] Ti contributes to an increase in the strength of a steel material, and when Ti is
contained, the Ti content may be 0% or more. To achieve the effect, when Ti is contained,
the content is preferably 0.005% or more, more preferably 0.008% or more. On the other
hand, a content of more than 0.1% results in saturation of the effect and causes an
increase in cost, so that when Ti is contained the Ti content is 0.1% or less. The
Ti content is preferably 0.08% or less, more preferably 0.06% or less. To reduce the
cost, the Ti content is still more preferably 0.05% or less. The Ti content is most
preferably 0.04% or less.
Cu: 0% to 1.0%
[0034] Cu is an element effective in improving the toughness and increasing the strength,
and when Cu is contained, the Cu content may be 0% or more, but to achieve these effects,
it is preferable to contain 0.01% or more, more preferably 0.05% or more. On the other
hand, an excessively high content results in lower weldability, and when Cu is contained,
the Cu content is 1.0% or less. The Cu content is preferably 0.95% or less, more preferably
0.9% or less. Still more preferably, the Cu content is 0.85% or less. Most preferably,
the Cu content is 0.5% or less.
Cr: 0% to 1.0%
[0035] Like Mn, Cr is an element effective in obtaining sufficient strength even at a low
C content, and when Cr is contained, the Cr content may be 0% or more, but to obtain
this effect, it is preferable to contain 0.01% or more, more preferably 0.05% or more.
On the other hand, an excessively high content results in lower SSCC resistance due
to excessive hardenability. Furthermore, weldability also deteriorates. Thus, when
Cr is contained, the Cr content is 1.0% or less. The Cr content is preferably 0.95%
or less. The Cr content is more preferably 0.9% or less, still more preferably 0.85%
or less.
Mo: 0% to 0.60%
[0036] Mo is an element effective in improving the toughness and increasing the strength
and is an element effective in improving the SSCC resistance and the HIC resistance.
When Mo is contained, the Mo content may be 0% or more and is preferably 0.01% or
more, more preferably 0.10% or more, to achieve the above effects. On the other hand,
an excessively high content results in lower SSCC resistance due to excessive hardenability.
Furthermore, weldability also deteriorates. Thus, when Mo is contained, the Mo content
is 0.60% or less. The Mo content is preferably 0.50% or less, more preferably 0.40%
or less, still more preferably 0.35% or less.
W: 0% to 1.0%
[0037] W contributes to an increase in the strength of a steel material. When W is contained,
the W content may be 0% or more and is preferably 0.01% or more to achieve the above
effect. On the other hand, a W content of more than 1.0% results in saturation of
the effect and causes an increase in cost, so that when W is contained, the W content
is 1.0% or less. The W content is preferably 0.9% or less, more preferably 0.8% or
less. To reduce the cost, 0.5% or less is still more preferred.
V: 0% to 0.10%, Zr: 0% to 0.050%, Mg: 0% to 0.01%, and REM: 0% to 0.01%
[0038] V is an element that can be optionally contained to increase the strength and toughness
of a steel material. When V is contained, the V content may be 0% or more, but the
effects of containing V are not sufficient at a V content of less than 0.01%, so that
the V content is preferably 0.01% or more. The V content is more preferably 0.03%
or more. On the other hand, more than 0.10% results in a weld with lower toughness,
so that when V is contained, 0.10% or less is preferred. The V content is preferably
0.09% or less. The V content is more preferably 0.07% or less, still more preferably
0.06% or less.
[0039] Zr, Mg, and REM are elements that can be optionally added to increase the toughness
through grain refinement or to increase cracking resistance through the control of
inclusion properties. When these elements are contained, each content may be 0% or
more, but the effects of containing these elements are insufficient at a content of
less than 0.0001%, so that each content is preferably 0.0001% or more, more preferably
0.0005% or more. More specifically, the Zr content is preferably 0.0001% or more.
The Zr content is more preferably 0.0005% or more. The REM content is preferably 0.0001%
or more. The REM content is more preferably 0.0005% or more. The Mg content is preferably
0.0001% or more. The Mg content is more preferably 0.0005% or more.
[0040] On the other hand, when the Zr content is more than 0.050%, and the Mg and REM contents
are more than 0.01%, the effects are saturated, so that when these are contained,
the Zr content is 0.050% or less, and the Mg and REM contents are 0.01% or less. More
specifically, when Zr is contained, the Zr content is 0.050% or less. The Zr content
is preferably 0.040% or less. The Zr content is more preferably 0.020% or less. When
REM is contained, the REM content is 0.01% or less. The REM content is preferably
0.009% or less. The REM content is more preferably 0.008% or less. When Mg is contained,
the Mg content is 0.01% or less. The Mg content is preferably 0.009% or less. The
Mg content is more preferably 0.008% or less.
B: 0% to 0.0020%
[0041] B is an element that improves hardenability, and contributes to an increase in the
strength of a steel material, suppresses coarsening of prior-austenite grains, and
improves various characteristics of the material. When B is contained, the B content
may be 0% or more and is preferably 0.0001% or more, more preferably 0.0008% or more,
to achieve the above effects. On the other hand, a B content of more than 0.0020%
results in saturation of the effect and causes an increase in cost, so that when B
is contained the B content is 0.0020% or less. The B content is preferably 0.0014%
or less. The B content is more preferably 0.0012% or less. To reduce the cost, 0.0010%
or less is still more preferred.
Ta: 0% to 0.2%
[0042] Ta is an element that forms a carbide or a nitride and contributes to an improvement
in the strength. When Ta is contained, the Ta content may be 0% or more and is preferably
0.0001% or more to achieve the above effect. More preferably, the Ta content is 0.0008%
or more. On the other hand, a content of more than 0.2% sometimes results in lower
toughness, so that when Ta is contained the Ta content is 0.2% or less. Ta is preferably
0.16% or less. Ta is more preferably 0.12% or less, still more preferably 0.10% or
less.
Hf: 0% to 0.2%, Re: 0% to 0.005%
[0043] These elements contribute to an increase in the strength of a steel material. To
achieve the above effect, when these elements are contained, each content is preferably
0.0001% or more, preferably 0.0010% or more. More specifically, when Hf is contained,
the Hf content is preferably 0.0001% or more. The Hf content is more preferably 0.0010%
or more. When Re is contained, the Re content is preferably 0.0001% or more. The Re
content is preferably 0.001% or more. On the other hand, when these elements are contained,
a Hf content of more than 0.2% or a Re content of more than 0.005% results in an increase
in an oxide, and aggregation reduces the hydrogen resistance, so that the Hf content
is 0.2% or less, and the Re content is 0.005% or less. More specifically, when Hf
is contained, the Hf content is 0.2% or less. The Hf content is preferably 0.18% or
less, more preferably 0.12% or less. When Re is contained, the Re content is 0.005%
or less. The Re content is preferably 0.004% or less, more preferably 0.003% or less.
Sn: 0% to 0.3%, Sb: 0% to 0.3%
[0044] These elements contribute to an increase in the strength and an improvement in the
hardenability of a steel material. When Sn and Sb are contained, the Sn and Sb contents
may be 0% or more and are each preferably 0.0001% or more to achieve the effects.
Preferably, it is 0.001% or more. More specifically, when Sn is contained, the Sn
content may be 0% or more and is preferably 0.0001% or more. The Sn content is more
preferably 0.001% or more. When Sb is contained, the Sb content may be 0% or more
and is preferably 0.0001% or more. The Sb content is more preferably 0.001% or more.
On the other hand, each content of more than 0.3% results in saturation of the effects
and an increase in cost, so that when Sn or Sb is contained the Sn or Sb content is
0.3% or less. To reduce the cost, 0.01% or less is preferred. Thus, when Sn is contained,
the Sn content is 0.3% or less. The Sn content is preferably 0.2% or less. The Sn
content is more preferably 0.1% or less. The Sn content is still more preferably 0.01%
or less. When Sb is contained, the Sb content is 0.3% or less. The Sb content is preferably
0.2% or less. The Sb content is more preferably 0.1% or less. The Sb content is still
more preferably 0.01% or less.
[0045] In the chemical composition of a steel material, the remainder other than these components
(elements) is composed of Fe and an incidental impurity element.
[0046] The metallic microstructure of a steel material according to the present invention
is described below.
Metallic Microstructure
[0047] Inclusions having aspect ratio of 2.0 or more and length of 10 µm or more: 15 pieces/100
mm
2 or less
An inclusion in a material is, for example, elongated MnS or cementite. These act
as a hydrogen accumulation source and cause a significant decrease in the HIC resistance
and a decrease in the hydrogen-induced crack growth threshold K
IH. Thus, the number of inclusions with an aspect ratio of 2.0 or more and a length
of 10 µm or more is 15 pieces/100 mm
2 or less. The number density of the inclusions is preferably 10 pieces/100 mm
2 or less. The lower limit may be, but is not limited to, 0 pieces/100 mm
2.
Retained austenite: 0% to 3% (preferred)
[0048] Retained austenite remaining in a steel material microstructure may act as a hydrogen
trap site, increases the amount of hydrogen in the steel, and increases hydrogen embrittlement
sensitivity. Furthermore, when a steel material or a steel pipe is used as a steel
structure, retained austenite is transformed into martensite due to stress loading
during use. Martensite, which is very hard, serves as a source or a propagation path
of HIC, and may significantly reduce the K
IH. In the present invention, a content of retained austenite of 3% or less improves
the K
IH. Thus, a content of retained austenite is preferably 3% or less. The content of retained
austenite is more preferably 2% or less, still more preferably 1% or less. The content
of retained austenite may be 0%.
[0049] Area fraction of bainite in range from surface of steel material (for steel pipe,
inner surface of steel pipe) to middle of sheet thickness: 90% or more (preferred)
[0050] As a material suitable for a line pipe, the steel microstructure of a steel material
is required to be a bainite microstructure to increase the tensile strength to 520
MPa or more. The bainite microstructure includes bainitic ferrite or granular bainite
that transforms during or after accelerated cooling contributing to transformation
strengthening, and also includes tempered bainite. A different microstructure, such
as ferrite, martensite, pearlite, a martensite-austenite constituent (MA), or retained
austenite, in the bainite microstructure reduces the strength, the toughness under
normal conditions (in the atmospheric environment), and the K
IH. Furthermore, presence of steel microstructures with different hardnesses cause stress
distribution in the steel material at the time of stress loading during use, acts
as a hydrogen accumulation source due to stress-induced diffusion, and reduces the
HIC resistance. Thus, an area fraction of bainite is preferably 90% or more. The area
fraction of bainite is more preferably 92% or more, still more preferably 95% or more.
The upper limit may be, but is not limited to, 100%.
[0051] Maximum grain size in range from surface of steel material (for steel pipe, inner
surface of steel pipe) to middle of sheet thickness: 25 µm or less
[0052] Although the average grain size is reduced to improve the toughness, the reduction
of the average grain size is limited when cooling is started at the Ar
3 point or higher. In the present disclosure, it is important to suppress the formation
of coarse crystal grains. Crystal grains with a large maximum grain size, if present,
induce occurrence of nonuniform strain in the material, promote accumulation of hydrogen,
and therefore reduce the fracture toughness in a hydrogen gas environment. In particular,
crystal grains with a maximum grain size of more than 25 µm in the range from the
inner surface of a steel material to the middle of the sheet thickness are likely
to accumulate strain around the grains, easily act as an origin of hydrogen fracture
and a propagation path, and significantly reduce the K
IH. Thus, the maximum grain size in the range from the inner surface of a steel material
to the middle of the sheet thickness should be 25 µm or less. The maximum grain size
in the range from the inner surface of a steel material to the middle of the sheet
thickness is preferably 24 µm or less, more preferably 22 µm or less, still more preferably
20 µm or less. Although the lower limit is not particularly limited, the maximum grain
size is preferably 4 µm or more. The grain size was measured in an area of 1 mm x
1 mm, and the grain size was defined as an area grain size (a weighted average when
a boundary with an orientation difference of 15 degrees or more is defined as a grain
boundary).
Hydrogen-induced crack growth threshold KIH in high-pressure hydrogen gas environment of 1 MPa or more: 80 MPa·m1/2 or more
[0053] For safe operation of a steel structure in an environment containing hydrogen, a
high-strength steel material according to the present disclosure has a hydrogen-induced
crack growth threshold K
IH of 80 MPa·m
1/2 or more in a high-pressure hydrogen gas environment of 1 MPa or more. Although the
upper limit is not particularly limited, the hydrogen-induced crack growth threshold
K
IH of the steel material is preferably 120 MPa·m
1/2 or less, more preferably 100 Pa·m
1/2 or less. The hydrogen-induced crack growth threshold K
IH refers to the plane-strain fracture toughness K
IC or its provisional value determined in accordance with ASTM E399 and ASTM E1820 in
a high-pressure hydrogen gas of 1 MPa or more, or the crack growth threshold or its
provisional value determined in accordance with ASTM E1681.
[0054] The sheet thickness of a steel material is preferably, but not limited to, 5 mm or
more. The sheet thickness is preferably 30 mm or less.
[0055] The chemical composition and metallic microstructure described above in the present
invention can provide a high hydrogen-induced crack threshold K
IH in a high-pressure hydrogen gas, and the present invention can be applied to a hydrogen
line pipe.
[0056] Furthermore, a high-strength steel material for a line pipe according to the present
invention can be produced by specifying the following production conditions, and the
production method and conditions are more specifically described below.
Molten steel step [average cooling rate of molten steel: 50°C/min or more (suitable
conditions)]
[0057] To reduce inclusions, it is also effective to reduce the S or O content. Because
the inclusions limited in the present invention aggregates in a cooling process of
molten steel, it is also effective to increase the average cooling rate of the molten
steel. Thus, the average cooling rate in the temperature range of 1500°C to 1000°C
is preferably 50°C/min or more. The average cooling rate is more preferably 60°C/min
or more, still more preferably 70°C/min or more. The upper limit is preferably, but
not limited to, 90°C/min or less.
Heating Step
[Heating temperature of cast steel: 1000°C to 1250°C]
[0058] A heating temperature of a cast steel, such as a billet or a slab, lower than 1000°C
results in insufficient diffusion of microsegregated impurity elements, such as C,
P, or S and an inhomogeneous material, and causes an increase in the number of inclusions,
nonuniform precipitations, and lower toughness. Thus, the heating temperature of a
cast steel is 1000°C or more. The heating temperature of a cast steel is preferably
1050°C or more, more preferably 1100°C or more. On the other hand, more than 1250°C
results in excessively coarse crystal grains and lower toughness. Thus, the heating
temperature of a cast steel is 1250°C or less. The heating temperature of a cast steel
is preferably 1200°C or less, more preferably 1150°C or less.
Rolling Step
[Total rolling reduction in recrystallization temperature range after heating cast
steel: 35% or more and 55% or less]
[0059] To reduce the maximum grain size of bainite, it is necessary to promote the recrystallization
of crystal grains and suppress the formation of coarse grains in hot rolling in a
recrystallization temperature range after heating a cast steel. When the total rolling
reduction in the recrystallization temperature range is less than 35%, recrystallization
is insufficient, and coarse grains remain. Thus, the total rolling reduction in the
recrystallization temperature range is 35% or more, preferably 38% or more. The total
rolling reduction in the recrystallization temperature range is more preferably 40%
or more, still more preferably 43% or more. On the other hand, when the total rolling
reduction in the recrystallization temperature range is more than 55%, the coarsening
of crystal grains can be suppressed, but the rolling reduction in the non-recrystallization
region is insufficient, and the crystal grains in the final product cannot be refined.
Thus, the total rolling reduction in the recrystallization temperature range is 55%
or less, preferably 52% or less. The total rolling reduction in the recrystallization
temperature range is more preferably 50% or less, still more preferably 48% or less.
The lower limit temperature Tnr of recrystallization can be determined, for example,
from the components of steel using the following formula. The surface temperature
of a steel sheet can be measured with a radiation thermometer or the like. The total
rolling reduction in the recrystallization temperature range refers to a total rolling
reduction at a temperature equal to or higher than the lower limit temperature Tnr
of recrystallization determined using the following formula.

[%X] represents the element X content (% by mass) of the steel.
[Rolling reduction in final rolling pass in recrystallization temperature range: 10%
or more]
[0060] In addition to setting the total rolling reduction in the recrystallization temperature
range to 35% or more and 55% or less, it is necessary to sufficiently ensure the rolling
reduction in the final rolling pass in the recrystallization temperature range and
sufficiently promote recrystallization, thereby starting rolling in a partial recrystallization
range in a state of uniform grains without coarse grains. When the rolling reduction
in the final rolling pass in the recrystallization temperature range is less than
10%, recrystallization is insufficient, and coarse grains grow during the holding
time from rough rolling to the start of finish rolling. Thus, the rolling reduction
in the final rolling pass in the recrystallization temperature range is 10% or more.
The rolling reduction in the final rolling pass in the recrystallization temperature
range is preferably 11% or more. The rolling reduction in the final rolling pass in
the recrystallization temperature range is more preferably 13% or more, still more
preferably 15% or more. Although the upper limit of the rolling reduction in the final
rolling pass in the recrystallization temperature range is not particularly limited,
a higher rolling reduction is more preferred. However, a rolling reduction of more
than 70% results in a significant decrease in productivity, so that the rolling reduction
is preferably 70% or less.
[Rolling reduction in final rolling pass at (recrystallization temperature - 80°C)
or more: 15% or more]
[0061] Since recrystallization partially occurs even after completion of rolling in the
recrystallization range, a further increase in the rolling reduction can promote recrystallization
and is effective in refining the top 20% of the grain size. Thus, the rolling reduction
in the final rolling pass at (recrystallization temperature - 80°C) or more is 15%
or more. The rolling reduction in the final rolling pass at (recrystallization temperature
- 80°C) or more is preferably 16% or more. The rolling reduction in the final rolling
pass at (recrystallization temperature - 80°C) or more is more preferably 18% or more,
still more preferably 20% or more. Although the upper limit of the rolling reduction
in the final rolling pass at (recrystallization temperature - 80°C) or more is not
particularly limited, a higher rolling reduction is more preferred. However, a rolling
reduction of more than 40% results in a significant decrease in productivity, so that
the rolling reduction is preferably 40% or less.
[0062] Rolling at a temperature lower than (recrystallization temperature - 80°C) is effective
for grain refinement because rolling at a low temperature introduces a large amount
of strain. Thus, rolling is preferably performed at a low temperature within the range
in which the cooling start temperature of controlled cooling can be complied with.
[0063] In the hot rolling step, although the finish rolling temperature is preferably as
low as possible to reduce the grain size, from the perspective of ensuring HISC resistance
in a high-pressure hydrogen environment, the finish rolling temperature should be
set so that the cooling start temperature of controlled cooling can be the Ar
3 point or higher in terms of a surface temperature of the hot-rolled steel sheet.
The term "Ar
3 point", as used herein, refers to a ferrite transformation start temperature during
cooling and can be determined, for example, from the components of steel using the
following formula. The surface temperature of a hot-rolled steel sheet can be measured
with a radiation thermometer or the like.
Ar3 (°C) = 910 - 310[%C] - 80[%Mn] - 20[%Cu] - 15[%Cr] - 55[%Ni] - 80[%Mo]
[%X] represents the element X content (% by mass) of the steel.
Cooling Step after Rolling (Controlled Cooling Step)
[Cooling start temperature of controlled cooling: Ar3 transformation point or higher in terms of surface temperature of hot-rolled steel
sheet]
[0064] When the steel sheet surface temperature at the start of cooling is lower than the
Ar
3 transformation point (the Ar
3 point), ferrite is formed before controlled cooling and greatly decreases the strength.
Thus, the surface temperature of a hot-rolled steel sheet at the start of cooling
is the Ar
3 transformation point or higher. The surface temperature of the hot-rolled steel sheet
at the start of cooling is preferably the Ar
3 transformation point + 20°C or more, more preferably the Ar
3 transformation point + 50°C or more. The surface temperature of a hot-rolled steel
sheet at the start of cooling is the temperature of the rear end of the hot-rolled
steel sheet at which the cooling start temperature is lowest. The surface temperature
of the hot-rolled steel sheet at the start of cooling is preferably the Ar
3 transformation point + 120°C or less, more preferably the Ar
3 transformation point + 80°C or less.
[Cooling start time difference between front end and rear end of hot-rolled steel
sheet in controlled cooling: 50 seconds or less]
[0065] When the time difference between a front end and a rear end of a hot-rolled steel
sheet in the rolling direction at the start of cooling is more than 50 seconds (s),
the temperature difference between the front end and the rear end at the start of
cooling increases, resulting in a larger temperature variation at the cooling stop,
a larger variation in Vickers hardness at 0.25 mm from a surface of a steel material
(for a steel pipe, the inner surface of the steel pipe), and causes lower HISC resistance.
Thus, the cooling start time difference between a front end and a rear end of a hot-rolled
steel sheet is 50 seconds or less. The cooling start time difference is preferably
45 seconds or less. The cooling start time difference is more preferably 40 seconds
or less, still more preferably 32 seconds or less. Although the hot-rolled steel sheet
length can be shortened to reduce the cooling start time difference, it reduces the
productivity. The cooling start time difference is therefore preferably reduced by
increasing the hot-rolled steel sheet line speed. The cooling start time difference
may be 0 seconds but is preferably 20 seconds or more from the perspective of productivity.
[Average Cooling Rate of Controlled Cooling]
[0066] Average cooling rate from 750°C to 550°C at middle of sheet thickness: 15°C/s to
50°C/s
When the average cooling rate from 750°C to 550°C at the middle of the sheet thickness
is less than 15°C/s, a predetermined bainite microstructure containing granular bainite
is not formed, and the strength decreases. Thus, the average cooling rate at the middle
of the sheet thickness is 15°C/s or more. From the perspective of reducing variations
in microstructure, the average cooling rate at the middle of the sheet thickness is
preferably 17°C/s or more. The average cooling rate at the middle of the sheet thickness
is preferably 20°C/s or more, more preferably 25°C/s or more. On the other hand, to
suppress variations in the grain size of the bainite microstructure, the average cooling
rate is 50°C/s or less. The average cooling rate is preferably 48°C/s or less, more
preferably 45°C/s or less. The average cooling rate is still more preferably 42°C/s
or less, most preferably 38°C/s or less. Further cooling of a hot-rolled steel sheet
temperature at the middle of the sheet thickness to 550°C or less is not particularly
limited. However, from the perspective of reducing variations in the microstructure
and grain size, the average cooling rate is preferably 15°C/s or more and 50°C/s or
less. That is, for further cooling to 550°C or less, the average cooling rate is preferably
15°C/s or more. The average cooling rate is more preferably 30°C/s or more, still
more preferably 35°C/s or more. For further cooling to 550°C or less, the average
cooling rate is preferably 50°C/s or less. The average cooling rate is more preferably
48°C/s or less, still more preferably 42°C/s or less. The average cooling rate to
550°C or less is an average value of the cooling rates from 550°C to 250°C.
[Cooling Stop Temperature: 250°C to 650°C]
[0067] When the cooling stop temperature at the middle of the sheet thickness after hot
rolling is more than 650°C, the material strength decreases greatly. Furthermore,
from the perspective of obtaining a uniform bainite microstructure, the cooling stop
temperature at the middle of the sheet thickness is 650°C or less. The cooling stop
temperature at the middle of the sheet thickness is preferably 620°C or less, more
preferably 615°C or less, still more preferably 600°C or less. On the other hand,
when the cooling stop temperature at the middle of the sheet thickness is less than
250°C, a quenching crack is likely to occur during cooling. Furthermore, to form a
uniform bainite microstructure, the cooling stop temperature is 250°C or more. The
cooling stop temperature at the middle of the sheet thickness is preferably 300°C
or more, more preferably 350°C or more, still more preferably 380°C or more. From
the perspective of reducing the amount of hydrogen in the steel, the cooling stop
temperature should be a predetermined temperature or higher. More specifically, hydrogen
in the steel is gradually released during cooling and this effect increases with the
temperature. However, an excessively low cooling stop temperature results in supercooling
and hydrogen remaining in the steel. Moreover, an excessively low cooling stop temperature
tends to result in the formation of retained austenite, which stores a larger amount
of hydrogen than other phases. Thus, the cooling stop temperature should be 250°C
or more to decrease the amount of hydrogen in the steel. After the cooling is stopped,
the steel may be allowed to cool and, to promote the formation of bainite, is preferably
gradually cooled until the temperature is lowered by approximately 50°C from the cooling
stop temperature.
[Dehydrogenation Treatment (Suitable Conditions)]
[0068] Hydrogen originally present in a steel material increases the acceleration of fatigue
crack growth and decreases the fatigue life. Thus, dehydrogenation treatment is preferably
performed to release hydrogen remaining after production. In the dehydrogenation treatment,
the amount of hydrogen in the steel can be reduced by holding the steel at a high
temperature for a certain period before using the product. The dehydrogenation treatment
can also be achieved by holding for an extended period even at room temperature. For
holding at room temperature, the holding time is prolonged and is preferably 96 hours
or more. Furthermore, the scale on the steel surface inhibits dehydrogenation and
is therefore preferably removed before dehydrogenation treatment. The holding time
R (s) is preferably determined from the sheet thickness or the wall thickness t (mm)
of a steel sheet or a steel pipe and the hydrogen diffusion coefficient D (mm·s
-1) in the steel at room temperature using the following formula (A).

[0069] The hydrogen diffusion coefficient varies depending on components contained and the
metallic microstructure and may range from, for example, 1 x 10
-5 to 5 x 10
-3 mm
2/s, more preferably 5 x 10
-4 mm
2/s or less. The dehydrogenation treatment step is performed before pipe production
or welding for connecting steel pipes. The dehydrogenation treatment is preferably
performed at a high temperature because the hydrogen diffusion coefficient D at a
high temperature is small and hydrogen is released quickly. At a high temperature,
the calculation may be performed using a diffusion coefficient D' (diffusion coefficient
at each temperature) at a temperature at which the value of D in the formula (A) is
held. On the other hand, an excessively high temperature T in the dehydrogenation
step results in a significant decrease in the material strength, and the dehydrogenation
treatment temperature is preferably 550°C or less. The dehydrogenation treatment temperature
T is more preferably 500°C or less. The dehydrogenation treatment temperature T is
still more preferably 400°C or less, most preferably 300°C or less. Furthermore, the
dehydrogenation treatment temperature T is preferably room temperature or higher for
the reason that the dehydrogenation treatment at a temperature lower than room temperature
increases the treatment time and cost. The dehydrogenation treatment temperature T
is more preferably 50°C or more. The dehydrogenation treatment temperature T is still
more preferably 100°C or more, most preferably 150°C or more. The dehydrogenation
treatment temperature T herein is the temperature of the atmosphere in the dehydrogenation
treatment step. The room temperature refers to 20°C ± 10°C.
[0070] In particular, when heating, it takes time for the temperature Tc at the middle of
the sheet thickness of a steel material or a steel pipe to reach the temperature of
the ambient in the dehydrogenation treatment step (dehydrogenation treatment temperature
T). Therefore, even if the holding time R (s) satisfies at the ambient temperature,
the dehydrogenation treatment may be insufficient if the dehydrogenation treatment
temperature T (ambient temperature) has not been reached at the middle of the sheet
thickness. Thus, it is preferable to hold for R (s) or more after the temperature
Tc at the middle of the sheet thickness reaches the target dehydrogenation treatment
temperature T. Furthermore, to achieve a predetermined fracture toughness in hydrogen
in hydrogen gas, it is necessary to appropriately adjust the amount of hydrogen in
a steel material in a surface layer portion and at the middle of the sheet thickness.
For this purpose, it is preferable to hold the steel material at the dehydrogenation
treatment temperature T (ambient temperature) for R (s) or more defined by the formula
(A), and it is further preferable to hold the steel material for the holding time
R (s) or more after the temperature Tc at the middle of the sheet thickness reaches
the target dehydrogenation treatment temperature T. In other words, at least the former
can appropriately control the amount of hydrogen in the steel material in the surface
layer portion of the steel material or the steel pipe, and when the latter is also
performed, the amount of hydrogen in the steel material from the surface layer portion
to the middle of the sheet thickness of the steel material or the steel pipe can be
appropriately controlled. The temperature Tc at the middle of the sheet thickness
may be actually measured with a thermocouple or the like or may be predicted using
a finite element method or the like.
[0071] The time and temperature in the dehydrogenation treatment step may include the temperature
and time applied at the time of heating in the pipe production step of an electric-resistance-welded
pipe, UOE, or the like, as described later. Furthermore, the scale on the steel surface
inhibits dehydrogenation and is therefore preferably removed before dehydrogenation
treatment. The removal method may be, for example, but is not limited to, physical
cleaning by high-pressure cleaning or a chemical method using a scale remover. If
the scale is removed by approximately 100 µm in thickness, the effects of scale removal
can be obtained.
Second Embodiment
[0072] Furthermore, a UOE steel pipe as an example of a steel pipe for a high-strength line
pipe can be produced by specifying the following production conditions, and the production
method and conditions are more specifically described below. The chemical composition,
the metallic microstructure, and the hydrogen-induced crack growth threshold K
IH of a UOE steel pipe are the same as those described for the steel sheet of the first
embodiment. Further, the molten steel step, the heating step, the hot rolling step,
the controlled cooling step after hot rolling, and the dehydrogenation treatment step
in the production method are performed in the same manner as described for the steel
material. The pipe production step after rolling is more specifically described below.
Pipe Production Step
[0073] A UOE steel pipe is produced by bending a hot-rolled steel sheet, more specifically,
groove-cutting an end portion of the hot-rolled steel sheet, forming the steel sheet
into a steel pipe shape by C-press, U-press, and O-press, seam-welding a butt joint
by inner surface welding and outer surface welding, and performing an expansion step
if necessary. The welding method may be any method that can achieve sufficient joint
strength and joint toughness and, from the perspective of good weld quality and production
efficiency, submerged arc welding is preferably used. Furthermore, a steel pipe produced
by press bending into a pipe shape and then seam-welding a butt joint can also be
subjected to expansion. Furthermore, when the inclusions are present in a weld heat-affected
zone after pipe production, the inclusions act as a hydrogen accumulation source in
the same manner as in the base metal zone and reduce the HIC resistance and K
IH. To reduce inclusions in a weld, it is also effective to reduce the S or O content.
Thus, the average cooling rate in the temperature range of 1500°C to 1000°C in a steel
pipe after welding is preferably 50°C/min or more. The average cooling rate is more
preferably 55°C/min or more, still more preferably 60°C/min or more. Although the
upper limit is not particularly limited, the average cooling rate is preferably 100°C/min
or less.
Third Embodiment
[0074] Furthermore, an electric-resistance-welded steel pipe as an example of a steel pipe
for a high-strength line pipe according to the present invention can be produced by
specifying the following production conditions, and the production method and conditions
are more specifically described below. The chemical composition, the metallic microstructure,
and the hydrogen-induced crack growth threshold K
IH of the steel material are the same as those described for the steel material of the
first embodiment. Further, the steps other than the cooling step after rolling and
the pipe production step (the molten steel step, the heating step, the hot rolling
step, and the dehydrogenation treatment step) in the production method are performed
in the same manner as described for the steel material.
Cooling Step after Rolling (Controlled Cooling Step)
[0075] The cooling start temperature of the controlled cooling and the average cooling rate
of the controlled cooling are the same as those described in the first embodiment.
[Cooling Stop Temperature: 250°C to 650°C]
[0076] When the cooling stop temperature at the middle of the sheet thickness after hot
rolling is more than 650°C, the material strength decreases greatly, and from the
perspective of obtaining a uniform bainite microstructure, the cooling stop temperature
at the middle of the sheet thickness is 650°C or less. The cooling stop temperature
at the middle of the sheet thickness is preferably 620°C or less, more preferably
615°C or less, still more preferably 600°C or less. On the other hand, when the cooling
stop temperature at the middle of the sheet thickness is less than 250°C, a quenching
crack is likely to occur during cooling. Thus, the cooling stop temperature at the
middle of the sheet thickness is 250°C or more. The cooling stop temperature at the
middle of the sheet thickness is preferably 300°C or more, more preferably 350°C or
more, still more preferably 380°C or more. To reliably suppress the formation of hard
microstructures on the surface of a steel sheet, the cooling stop temperature at the
middle of the sheet thickness is most preferably 450°C or more. After the cooling
is stopped, the steel may be allowed to cool and, to promote the formation of bainite,
is preferably gradually cooled until the temperature is lowered by approximately 50°C
from the cooling stop temperature.
[0077] A hot-rolled steel sheet thus produced is then coiled. The coiling temperature is
preferably 650°C or less. The coiling temperature is more preferably 620°C or less,
still more preferably 615°C or less, still more preferably 600°C or less. The lower
limit of the coiling temperature is preferably 250°C or more, more preferably 300°C
or more, still more preferably 350°C or more, most preferably 380°C or more.
Pipe Production Step
[0078] An electric-resistance-welded steel pipe as an example of the present invention is
produced by forming a cylindrical shape by cold roll forming and butt-welding both
circumferential end portions of the cylindrical shape. An electric-resistance-welded
steel pipe may also be produced by forming an electric-resistance-welded steel pipe
material (electric-resistance-welded steel pipe) using a sizing roll satisfying the
following formula (1) (a sizing step) and applying an internal pressure p (MPa) satisfying
the following formula (2) to the inner surface of the electric-resistance-welded steel
pipe material (an internal pressure applying step). The term "cylindrical shape" means
that the cross section of the pipe has a "C" shape.
Diameter (mm) of sizing roll ≥ Thickness (mm) of hot-rolled steel sheet/0.020 (1)
[0079] The thickness of a hot-rolled steel sheet refers to the thickness of the hot-rolled
steel sheet before the sizing step.

[0080] X = (wall thickness (mm) of electric-resistance-welded steel pipe material/radius
(mm) of electric-resistance-welded steel pipe material) x yield strength (MPa) of
electric-resistance-welded steel pipe material
[0081] The internal pressure can be applied, for example, by sealing a pipe end with a packing
made of a rubber material and applying water pressure to the inside of the pipe. To
stabilize the shape, if necessary, a die with a desired diameter may be used as an
outer frame.
[0082] An electric-resistance-welded steel pipe material as an example of a steel pipe according
to the present invention preferably has a wall thickness of 5 mm or more. The electric-resistance-welded
steel pipe material preferably has a wall thickness of 30 mm or less. Although the
radius of the electric-resistance-welded steel pipe material may have any upper limit,
the load on the facilities increases with the radius, and the electric-resistance-welded
pipe material therefore preferably has a radius of 400 mm or less. The electric-resistance-welded
pipe material preferably has a radius of 200 mm or more. The electric-resistance-welded
steel pipe material preferably has a yield strength of 480 MPa or more to withstand
pipeline operation gas pressures. The yield strength is more preferably 500 MPa or
more. On the other hand, to avoid an increase in hydrogen embrittlement sensitivity,
the yield strength is preferably 560 MPa or less. The yield strength is more preferably
550 MPa or less.
[0083] In the sizing step, passage through rolls causes bending deformation along the roll
shape in the pipe axis direction and generates residual stress in the pipe axis direction.
The absolute value of the residual stress in the pipe axis direction increases with
the bending strain in the bending deformation. The bending strain increases as the
diameter of the sizing roll decreases and as the thickness of the hot-rolled steel
sheet increases. Thus, in the present invention, from the perspective of reducing
the shear residual stress, the diameter of the sizing roll satisfies the formula (1)
to reduce the absolute value of the residual stress in the pipe axis direction. When
the sizing roll has a diameter smaller than the right side of the formula (1), the
shear residual stress intended in the present invention cannot be obtained. Although
the diameter of the sizing roll may have any upper limit, the load on the facilities
increases with the sizing roll, and the sizing roll therefore preferably has a diameter
of 2000 mm or less.
[0084] In the internal pressure applying step, the electric-resistance-welded steel pipe
material is expanded to generate tensile stress in the circumferential direction of
the pipe and reduce the absolute value of residual stress in the circumferential direction
of the pipe. As the internal pressure p (MPa) in the internal pressure applying step
increases, the absolute value of the residual stress in the circumferential direction
of the pipe decreases. The tensile stress generated in the circumferential direction
of the pipe increases as the radius of the steel pipe increases and as the wall thickness
of the steel pipe decreases.
[0085] The left side (X) of the formula (2) corresponds to the internal pressure p when
the tensile stress generated in the circumferential direction of the pipe is equal
to the yield stress of the electric-resistance-welded steel pipe material. In the
present invention, from the perspective of reducing the shear residual stress, the
internal pressure p is larger than the left side (X) of the formula (2) to expand
the electric-resistance-welded steel pipe material to the plastic region in order
to reduce the absolute value of the residual stress in the pipe axis direction. On
the other hand, when the internal pressure p exceeds the right side (X x 1.5) of the
formula (2), the absolute value of the residual stress in the circumferential direction
of the pipe decreases, but the amount of work hardening due to expansion increases
excessively, the dislocation density on the pipe surface increases, and the fracture
toughness in hydrogen decreases.
[0086] As partially described above, regarding a high-strength steel pipe, a high-strength
steel pipe for a line pipe for sour gas service (a UOE steel pipe, an electric-resistance-welded
steel pipe, a spiral steel pipe, or the like) with high material uniformity in the
steel sheet suitable for transportation of crude oil or natural gas can be produced
by forming a high-strength steel material according to the present disclosure into
a tubular shape by press bending, roll forming, UOE forming, or the like and then
welding a butt joint. Furthermore, a high-strength steel sheet according to the present
disclosure can be used for a steel pipe to produce a steel pipe with high HISC resistance
even when a high hardness region of a weld is present.
EXAMPLE 1
[0087] The present invention is more specifically described in the following examples. The
examples are preferred examples of the present invention, and the present invention
is not limited to these examples.
[0088] Slabs with the chemical compositions shown in Tables 1-1 and 1-2 were prepared, were
hot-rolled, and were subjected to controlled cooling and dehydrogenation treatment
to produce steel materials. The steel materials were formed into steel pipes. The
production conditions are shown in Tables 2-1 and 2-2. For Nos. 2 to 6, 12 to 22,
35, and 37, steel pipes were formed by the pipe production step of bending each steel
material (hot-rolled steel sheet) and butt-welding both end portions thereof. For
Nos. 7 to 11, 23 to 33, 36, and 38, steel pipes were formed by the pipe production
step of forming each steel material (hot-rolled steel sheet) into a cylindrical shape
by cold roll forming and subjecting both circumferential end portions of the cylindrical
shape to butt electric resistance welding. In Nos. 1 and 34, the steel materials were
used as they were. Tables 3-1 and 3-2 show the evaluation results of the metallic
microstructure and the material quality of each of the steel materials and steel pipes
thus produced. The evaluation method is described below.
Retained Austenite Measurement
[0089] A sample for metallic microstructure observation was taken from a central portion
of the sheet width in a central portion in the longitudinal direction of each of the
steel materials and the steel pipes thus produced. A cross section parallel to the
longitudinal direction was buffed as an observation surface. The surface layer was
then removed by chemical polishing using picric acid etching, and X-ray diffractometry
was performed. More specifically, a Co-Kα radiation source was used for an incident
X-ray, and the area fraction of retained austenite was calculated from the intensity
ratios of the (200), (211), and (220) planes of ferrite to the (200), (220), and (311)
planes of austenite.
Calculation of Maximum Grain Size and Area Fraction of Bainite
[0090] A sample for metallic microstructure observation was taken from a central portion
of the sheet width of each of the steel materials and the steel pipes thus produced,
and a cross section of the sample parallel to the rolling longitudinal direction was
used as a surface to be observed. The surface to be observed was mirror-polished and
etched with colloidal silica, and crystal data were collected by an electron backscatter
diffraction (EBSD) method in a visual field of 1 mm x 1 mm at the center of the sample
(measuring step: 0.8 µm). The grain size was defined as an area grain size (a weighted
average when a boundary with an orientation difference of 15 degrees or more is defined
as a grain boundary). Each grain size was determined from the crystal data to determine
the maximum grain size. For the area fraction, the surface to be observed was etched
with a 3% by volume nital solution, and a scanning electron microscope photograph
was taken at an appropriate magnification in the range of 1000 to 5000 times to observe
bainite. The bainite was visually identified by comparison with the microstructure
photograph of Non Patent Literature 1, and the microstructure fraction was determined
as an area fraction of bainite by binarizing the bainite and the other region in the
SEM photograph based on the above identification and determining the area fraction
by image analysis.
Observation of Inclusions and Calculation of Number Density
[0091] A sample for metallic microstructure observation was taken from a central portion
of the sheet width in a central portion in the longitudinal direction of each of the
steel materials and the steel pipes thus produced, and a cross section of the sample
parallel to the rolling longitudinal direction was used as a surface to be observed.
The surface to be observed was mirror-polished, was then etched with colloidal silica,
and was observed with a scanning electron microscope (SEM) in a visual field of 10
mm x 10 mm at the center of the sample. The observation magnification ranges from
2000 to 5000 times, and the average of three visual fields was taken as the number
density of inclusions.
Tensile Strength (TS)
[0092] JIS No. 14 proportional test pieces (parallel portion diameter: 7 mm, gauge length:
35 mm) were taken in accordance with JIS Z 2201 from the steel materials and the steel
pipes thus produced, and the tensile strength was measured.
Hydrogen Temperature-Programmed Analysis
[0093] The amount of hydrogen remaining in the steel was measured by thermal desorption
spectrometry using a low-temperature programmed hydrogen analyzer <gas chromatograph
type> (JTF-20AL). The thermal desorption spectrometry was performed in the temperature
range of room temperature to 400°C at a heating rate of 200°C/h, and the sum total
thereof was taken as the amount of hydrogen. The specimen has a cylindrical shape
with 30 mm in length and 7Φ in diameter in the longitudinal direction of the steel
pipe at the quarter thickness position of the steel material and at the quarter thickness
position from the inner surface of the steel pipe. The amount of hydrogen is the amount
of H shown in Tables 1-1 and 1-2 before being subjected to a high-pressure hydrogen
fatigue test as explained in the item described later.
Fracture Toughness Test in High-Pressure Hydrogen Gas
[0094] The test was performed in accordance with ASTM E1820 in a hydrogen gas (including
100% hydrogen) at room temperature (20°C ± 10°C) with a pressure of 25 MPa or in a
natural gas (the main components are hydrocarbons, such as methane and ethane) mixed
atmosphere having the above temperature and pressure and containing hydrogen at a
hydrogen partial pressure of 1 MPa or more. A CT test specimen (thickness: 12.7 mm,
width: 25.4 mm) was used as a test specimen and was taken in a direction in which
the machine notch introduction direction was parallel to the rolling direction of
the steel material. A fatigue precrack was introduced in the atmosphere, and the conditions
included frequency: 1 Hz, cyclic loading waveform: sine wave, control method: K-value
control, and stress ratio R: 0.1. The atmosphere was then changed to hydrogen gas
or a hydrogen gas + natural gas mixed atmosphere. A fracture toughness test was performed
by an unloading-elastic compliance method using a single test specimen. The crosshead
displacement speed at the time of loading was 0.002 mm/s.
[0095] The evaluation results are shown in Tables 3-1 and 3-2. All of the steel materials
and steel pipes satisfying Inventive examples of the present invention had high fracture
toughness resistance in hydrogen with a hydrogen-induced crack growth threshold K
IH of 80 MPa·m
1/2 or more and had a tensile strength of 520 MPa or more. The steel pipes in Tables
3-1 and 3-2 also showed the same results as the steel materials.
[Table 3-1]
Steel pipe No. |
Steel material No. |
Steel No. |
Area fraction of retained austenite (%) |
B fraction (%) |
Maximum grain size of bainite (µm) |
Number density of inclusions (/100 mm2) |
Tensile strength (MPa) |
Hydrogen-induced crack growth threshold KIH (MPa √m) |
Notes |
Base metal zone |
1 |
1 |
1 |
0.0 |
98.6 |
22 |
15 |
699 |
129 |
Inventive example |
2 |
2 |
2 |
0.2 |
92.5 |
23 |
12 |
561 |
159 |
Inventive example |
3 |
3 |
3 |
0.5 |
93.4 |
19 |
33 |
700 |
75 |
Comparative example |
4 |
4 |
4 |
0.0 |
98.1 |
21 |
12 |
552 |
170 |
Inventive example |
5 |
5 |
5 |
0.9 |
95.9 |
18 |
15 |
590 |
129 |
Inventive example |
6 |
6 |
6 |
1.0 |
95.3 |
55 |
14 |
530 |
62 |
Comparative example |
7 |
7 |
7 |
0.3 |
98.1 |
51 |
12 |
702 |
60 |
Comparative example |
8 |
8 |
8 |
0.0 |
90.6 |
19 |
9 |
662 |
100 |
Inventive example |
9 |
9 |
9 |
0.8 |
92.0 |
19 |
15 |
543 |
167 |
Inventive example |
10 |
10 |
10 |
0.9 |
93.4 |
22 |
9 |
559 |
131 |
Inventive example |
11 |
11 |
11 |
0.4 |
92.0 |
22 |
10 |
576 |
119 |
Inventive example |
12 |
12 |
12 |
2.5 |
99.9 |
39 |
9 |
699 |
59 |
Comparative example |
13 |
13 |
13 |
0.0 |
91.8 |
24 |
11 |
653 |
99 |
Inventive example |
14 |
14 |
14 |
0.0 |
97.1 |
22 |
9 |
626 |
100 |
Inventive example |
15 |
15 |
15 |
0.0 |
93.6 |
14 |
10 |
564 |
137 |
Inventive example |
16 |
16 |
16 |
2.1 |
98.9 |
41 |
13 |
756 |
59 |
Comparative example |
17 |
17 |
17 |
0.0 |
94.5 |
25 |
15 |
534 |
153 |
Inventive example |
18 |
18 |
18 |
0.5 |
96.1 |
18 |
15 |
545 |
157 |
Inventive example |
19 |
19 |
19 |
0.0 |
90.5 |
21 |
12 |
623 |
122 |
Inventive example |
20 |
20 |
20 |
0.0 |
93.7 |
19 |
11 |
647 |
120 |
Inventive example |
Underline: outside the scope of the present invention.
B: bainite |
[Table 3-2]
Steel pipe No. |
Steel material No. |
Steel No. |
Area fraction of retained austenite (%) |
B fraction (%) |
Maximum grain size of bainite (µm) |
Number density of inclusions (/100 mm2) |
Tensile strength (MPa) |
Hydrogen-induced crack growth threshold KIH (MPa √m) |
Notes |
Base metal zone |
21 |
21 |
21 |
0.0 |
90.1 |
17 |
9 |
586 |
140 |
Inventive example |
22 |
22 |
22 |
0.2 |
94.0 |
24 |
13 |
525 |
160 |
Inventive example |
23 |
23 |
23 |
0.0 |
97.0 |
23 |
9 |
548 |
149 |
Inventive example |
24 |
24 |
24 |
1.5 |
92.9 |
40 |
14 |
530 |
58 |
Comparative example |
25 |
25 |
25 |
0.0 |
90.2 |
20 |
10 |
587 |
124 |
Inventive example |
26 |
26 |
26 |
0.0 |
92.8 |
19 |
11 |
554 |
137 |
Inventive example |
27 |
27 |
27 |
0.0 |
92.7 |
17 |
9 |
503 |
90 |
Comparative example |
28 |
28 |
28 |
1.2 |
91.1 |
29 |
8 |
530 |
70 |
Comparative example |
29 |
29 |
29 |
1.1 |
82.1 |
26 |
13 |
501 |
69 |
Comparative example |
30 |
30 |
30 |
0.0 |
93.0 |
30 |
14 |
556 |
70 |
Comparative example |
31 |
31 |
31 |
0.0 |
90.9 |
18 |
10 |
520 |
82 |
Inventive example |
32 |
32 |
32 |
1.7 |
93.6 |
24 |
15 |
700 |
81 |
Inventive example |
33 |
33 |
33 |
0.3 |
99.3 |
19 |
15 |
579 |
81 |
Inventive example |
34 |
34 |
34 |
3.9 |
90.1 |
17 |
12 |
593 |
61 |
Comparative example |
35 |
35 |
35 |
0.0 |
90.9 |
17 |
25 |
609 |
69 |
Comparative example |
36 |
36 |
36 |
0.2 |
94.0 |
19 |
27 |
525 |
59 |
Comparative example |
37 |
37 |
37 |
0.9 |
93.2 |
21 |
9 |
582 |
102 |
Inventive example |
38 |
38 |
38 |
1.0 |
90.4 |
18 |
13 |
601 |
99 |
Inventive example |
Underline: outside the scope of the present invention.
B: bainite |
EXAMPLE 2
[0096] Examples that have verified the advantages of the present invention are described
below. In the following Examples, steel materials and steel pipes were produced under
the following production conditions and were characterized. The steel Nos. 2, 4, 8,
14, 22, and 33 shown in Tables 1-1 and 1-2 used in Example 1 were used, up to the
controlled cooling step was performed under the same conditions as the steel pipes
2, 4, 8, 14, 22, and 33 shown in Example 1 (Tables 2-1 and 2-2). Steel pipe forming
was also performed under the same conditions as Example 1, and the characteristics
were evaluated while the dehydrogenation treatment conditions were changed. Table
4 shows the results.
[0097] The dehydrogenation treatment of the steel pipes Nos. 2, 4, 8, 14, 22, and 33 in
Example 1 was performed at a dehydrogenation treatment temperature T (ambient temperature)
and time shown in Tables 2-1 and 2-2. As shown in Table 4, the dehydrogenation holding
time t corresponds to Y and the retention time tc at the temperature Tc at the middle
of the sheet thickness corresponds to N, respectively in Table 4.
[0098] For the steel pipes Nos. 2A, 4A, 8A, 14A, 22A, and 33A, the dehydrogenation treatment
temperature T was the temperature shown in Table 4, and the holding time tc after
the temperature Tc at the middle of the sheet thickness reached the dehydrogenation
treatment temperature T shown in Table 4 satisfied the formula (A).
[0099] For the steel pipes Nos. 2B, 4B, 8B, 14B, 22B, and 33B, the dehydrogenation treatment
temperature T is the temperature shown in Table 4, but neither the holding time t
at the ambient temperature nor the holding time tc after the temperature Tc at the
middle of the sheet thickness reaches the dehydrogenation treatment temperature T
satisfy the formula (A).
[0100] In Table 4, "Dehydrogenation holding time t is Y" means that the dehydrogenation
treatment temperature T (ambient temperature) is a predetermined temperature and the
holding time t satisfies the formula (A), and "Dehydrogenation holding time t is N"
means that the dehydrogenation treatment temperature T (ambient temperature) is a
predetermined temperature, but the holding time t does not satisfy the formula (A).
Furthermore, "Holding time tc at steel material center temperature Tc is Y" means
that the holding time tc after the temperature Tc at the middle of the sheet thickness
reaches a predetermined temperature satisfies the formula (A), and "Holding time tc
at steel material center temperature Tc is N" means that the temperature Tc at the
middle of the sheet thickness reaches a predetermined temperature, but the holding
time tc after Tc reaches a predetermined temperature does not satisfy the formula
(A).
[0101] The examination of the fracture toughness in hydrogen and the tensile strength and
the evaluation of the microstructure and inclusions were performed in the same manner
as in Example 1.
[0102] All of the examples of the present invention satisfied the conditions of a hydrogen-induced
crack growth threshold K
IH of 80 MPa·m
1/2 or more and a tensile strength of 520 MPa or more. Among them, the fracture toughness
resistance in hydrogen was better when the dehydrogenation treatment was performed
under more suitable conditions.
[0103] The steel pipes in Table 4 also showed the same results as the steel materials.
[Table 4]
Steel pipe No. |
Steel material No. |
Steel No. |
Dehydrogenation treatment temperature T (°C) |
Dehydrogenation holding time t |
Holding time tc at steel material center temperature Tc |
Area fraction of retained austenite (%) |
B fraction % () |
Maximum grain size of bainite (µm) |
Number density of inclusions (/100 mm2) |
Tensile strength (MPa) |
Hydrogen-induced crack growth threshold KIH (MPa √m) base metal zone |
Notes |
2A |
2A |
2 |
200 |
Y |
Y |
0.2 |
92.5 |
23 |
12 |
540 |
199 |
Inventive example |
2 |
2 |
2 |
200 |
Y |
N |
0.2 |
92.5 |
23 |
12 |
561 |
159 |
Inventive example |
2B |
2B |
2 |
200 |
N |
N |
0.2 |
92.5 |
23 |
12 |
570 |
134 |
Inventive example |
4A |
4A |
4 |
50 |
Y |
Y |
0.0 |
98.1 |
21 |
12 |
552 |
188 |
Inventive example |
4 |
4 |
4 |
50 |
Y |
N |
0.0 |
98.1 |
21 |
12 |
552 |
170 |
Inventive example |
4B |
4B |
4 |
50 |
N |
N |
0.0 |
98.1 |
21 |
12 |
552 |
132 |
Inventive example |
8A |
8A |
8 |
25 |
Y |
Y |
0.0 |
90.6 |
19 |
9 |
662 |
151 |
Inventive example |
8 |
8 |
8 |
25 |
Y |
N |
0.0 |
90.6 |
19 |
9 |
662 |
100 |
Inventive example |
8B |
8B |
8 |
25 |
N |
N |
0.0 |
90.6 |
19 |
9 |
662 |
88 |
Inventive example |
14A |
14A |
14 |
500 |
Y |
Y |
0.0 |
97.1 |
22 |
9 |
589 |
141 |
Inventive example |
14 |
14 |
14 |
500 |
Y |
N |
0.0 |
97.1 |
22 |
9 |
626 |
100 |
Inventive example |
14B |
14B |
14 |
500 |
N |
N |
0.0 |
97.1 |
22 |
9 |
641 |
89 |
Inventive example |
22A |
22A |
22 |
80 |
Y |
Y |
0.2 |
94.0 |
24 |
13 |
525 |
179 |
Inventive example |
22 |
22 |
22 |
80 |
Y |
N |
0.2 |
94.0 |
24 |
13 |
525 |
160 |
Inventive example |
22B |
22B |
22 |
80 |
N |
N |
0.2 |
94.0 |
24 |
13 |
525 |
120 |
Inventive example |
33A |
33A |
33 |
500 |
Y |
Y |
0.3 |
99.3 |
19 |
15 |
540 |
139 |
Inventive example |
33 |
33 |
33 |
500 |
Y |
N |
0.3 |
99.3 |
19 |
15 |
579 |
81 |
Inventive example |
33B |
33B |
33 |
500 |
N |
N |
0.3 |
99.3 |
19 |
15 |
588 |
80 |
Inventive example |