Technical Field
[0001] The present invention relates to a ferritic stainless steel and particularly relates
to a ferritic stainless steel that has excellent creep resistance and thermal fatigue
resistance and that is suitable for use in exhaust system components used at high
temperatures, such as automotive and motorcycle exhaust pipes and converter cases
as well as exhaust ducts in thermal power generation plants.
Background Art
[0002] Excellent heat resistance is required for automotive exhaust system components, such
as exhaust manifolds, exhaust pipes, converter cases, and mufflers/silencers. Heat
resistance includes several properties, such as thermal fatigue resistance, high-temperature
fatigue resistance, high-temperature strength (high-temperature proof stress), oxidation
resistance, creep resistance, and hot salt corrosion resistance. Among these properties,
Thermal fatigue resistance is one of the most important properties among these properties
included in heat resistance. Exhaust system components are subjected to repeated heating
and cooling as an engine is started and stopped. On such an occasion, thermal expansion
and contraction of the exhaust system components is restrained due to peripheral parts
connected thereto, thereby generating thermal strain in the materials per se. A low-cycle
fatigue phenomenon in which repeated such thermal strain results in failure is referred
to as thermal fatigue.
[0003] As a material for the above-mentioned components in which excellent thermal fatigue
resistance are required, a ferritic stainless steel, such as Type 429, which contains
Nb and Si (14%Cr-0.9%Si-0.4%Nb steel), is commonly used today. However, as the engine
performance improves, an exhaust gas temperature has risen to a temperature exceeding
900°C. In such a case, Type 429 cannot fully satisfy, in particular, required thermal
fatigue resistance.
[0004] As materials that can resolve this problem, for example, SUS444 (19%Cr-0.5%Nb-2%Mo)
defined in JIS G 4305, which is a ferritic stainless steel having a high-temperature
proof stress enhanced by addition of Nb and Mo; and a ferritic stainless steel added
with Nb, Mo, and W have been developed (see, for example, Patent Literature 1)
Citation List
Patent Literature
[0005] PTL 1: Japanese Unexamined Patent Application Publication No.
2004-018921
Summary of Invention
Technical Problem
[0006] An exhaust gas temperature has a tendency to rise for the purpose of complying with
tightening emission control regulations and/or improving fuel efficiency in these
days. Consequently, even SUS444 or the like exhibits unsatisfactory heat resistance
in some cases, in particular, thermal fatigue resistance. Moreover, stainless steel
readily causes creep deformation when an exhaust gas temperature rises beyond 900°C
and thus also needs creep resistance.
[0007] SUS444 has the highest level of heat resistance among ferritic stainless steels,
but the heat resistance is not necessarily satisfactory when an exhaust gas temperature
rises as a result of recent tightening of emission control regulations and/or improvements
in fuel efficiency. As an exhaust gas temperature rises, an exhaust system component
undergoes large thermal expansion upon heating. Consequently, further severe thermal
strain is applied and a ferritic stainless steel used for the exhaust system component
readily undergoes thermal fatigue failure. Further, a ferritic stainless steel tends
to cause creep deformation when held for a prolonged time in a high-temperature range.
Once creep deformation occurs, a portion thinned by creep deformation reaches fracture
as it acts a starting point of fracture. Accordingly, it is also needed to improve
creep resistance.
[0008] As described above, according to conventional techniques including SUS444, it was
impossible to obtain a ferritic stainless steel that has satisfactory thermal fatigue
resistance even when an exhaust gas temperature rises. Moreover, creep resistance,
which are required particularly when an exhaust gas temperature exceeds 900°C, have
not been evaluated sufficiently.
[0009] In view of the above, an object of the present invention is to resolve the above-mentioned
problems and to provide a ferritic stainless steel having excellent creep resistance
and thermal fatigue resistance.
[0010] In the present invention, the expression "excellent creep resistance" means that
a rupture time is better than that of SUS444 when a creep test is performed at 900°C.
Moreover, the expression "excellent thermal fatigue resistance" means that resistance
better than SUS444 are exhibited, specifically, a thermal fatigue life is better than
that of SUS444 when the temperature is elevated and lowered repeatedly between 200°C
and 950°C.
Solution to Problem
[0011] For the purpose of developing a ferritic stainless steel that has better creep resistance
and better thermal fatigue resistance than SUS444, the present inventors continued
intensive studies on how various elements affect creep resistance and thermal fatigue
resistance.
[0012] As a result, it was found that high-temperature strength increases in a wide temperature
range and thermal fatigue resistance is improved by containing, in mass%, 0.30 to
0.80% of Nb and 1.80 to 2.50% of Mo in the total content of Nb and Mo of 2.3 to 3.0%.
Further, it was also found that creep resistance is improved by containing Sb in a
range of 0.002 to 0.50 mass%.
[0013] On the basis of the above findings, the present invention has been completed by satisfying
a specific chemical composition that contains all of Cr, Nb, Mo, and Sb in appropriate
amounts. Although the above-mentioned elements are important in the present invention,
it is needed to adjust all the essential elements to predetermined contents in order
to achieve the effects of the present invention.
[0014] The present invention is summarized as follows.
- [1] A ferritic stainless steel having a chemical composition containing, in mass%,
C: 0.020% or less, Si: 0.1 to 1.0%, Mn: 0.05 to 0.60%, P: 0.050% or less, S: 0.008%
or less, Ni: 0.02 to 0.60%, Al: 0.001 to 0.25%, Cr: 18.0 to 20.0%, Nb: 0.30 to 0.80%,
Mo: 1.80 to 2.50%, N: 0.015% or less, and Sb: 0.002 to 0.50%, with the balance being
Fe and inevitable impurities, and satisfying the following expression (1);
Nb + Mo: 2.3 to 3.0% (1)
where Nb and Mo in expression (1) represent the contents (mass%) of the respective
elements.
- [2] The ferritic stainless steel according to [1], where the chemical composition
further contains, in mass%, one or two or more selected from Ti: 0.01 to 0.16%, Zr:
0.01 to 0.50%, Co: 0.01 to 0.50%, B: 0.0002 to 0.0050%, V: 0.01 to 1.0%, W: 0.01 to
5.0%, Cu: 0.01 to 0.40%, and Sn: 0.001 to 0.005%.
- [3] The ferritic stainless steel according to [1] or [2], where the chemical composition
further contains, in mass%, one or two selected from Ca: 0.0002 to 0.0050% and Mg:
0.0002 to 0.0050%.
- [4] The ferritic stainless steel according to any one of [1] to [3], where the ferritic
stainless steel is used for an exhaust manifold whose temperature is elevated to 700°C
or higher by an exhaust gas from an engine. Advantageous Effects of Invention
[0015] According to the present invention, it is possible to provide a ferritic stainless
steel having better creep resistance and better thermal fatigue resistance than SUS444
(JIS G 4305). Accordingly, the ferritic stainless steel of the present invention can
be suitably used for exhaust system components of automobiles and so forth.
Brief Description of Drawings
[0016]
[Fig. 1] Fig. 1 illustrates a creep test specimen.
[Fig. 2] Fig. 2 illustrates a thermal fatigue test specimen.
[Fig. 3] Fig. 3 illustrates the temperature and restraint conditions in a thermal
fatigue test.
Description of Embodiments
[0017] Hereinafter, embodiments of the present invention will be described. However, the
present invention is not limited to the following embodiments.
[0018] A ferritic stainless steel of the present invention contains, in mass%, C: 0.020%
or less, Si: 0.1 to 1.0%, Mn: 0.05 to 0.60%, P: 0.050% or less, S: 0.008% or less,
Ni: 0.02 to 0.60%, Al: 0.001 to 0.25%, Cr: 18.0 to 20.0%, Nb: 0.30 to 0.80%, Mo: 1.80
to 2.50%, N: 0.015% or less, and Sb: 0.002 to 0.50%, with the balance being Fe and
inevitable impurities, and satisfies the following expression (1);
Nb + Mo: 2.3 to 3.0% (1)
where Nb and Mo in expression (1) represent the contents (mass%) of the respective
elements.
[0019] In the present invention, the balance in the chemical composition is extremely important.
By satisfying the above-described combinations of the chemical composition, it is
possible to obtain a ferritic stainless steel having better creep resistance and better
thermal fatigue resistance than SUS444. Meanwhile, even if one of the essential elements
(C, Si, Mn, Ni, Al, Cr, Nb, Mo, N, Sb) in the chemical composition falls outside the
above-mentioned content range, it is impossible to achieve expected creep resistance
and thermal fatigue resistance.
[0020] Next, the chemical composition of the ferritic stainless steel of the present invention
will be described. Hereinafter, the sign "%" as a unit denoting the content of each
element means mass% unless otherwise stated.
C: 0.020% or less
[0021] C is an element effective for increasing the strength of steel, but toughness and
formability remarkably deteriorate when C content exceeds 0.020%. Moreover, C combines
with Nb, which is important in the present invention, and increases the amount of
the resulting carbide. Consequently, the effect of improving thermal fatigue resistance
and creep resistance by Nb described hereinafter diminishes. Accordingly, C content
is set to 0.020% or less. From a viewpoint of ensuring formability, C content is set
to preferably 0.010% or less and more preferably 0.008% or less. Meanwhile, from a
viewpoint of ensuring the strength as an exhaust system component, C content is set
to preferably 0.001% or more, more preferably 0.003% or more, and further preferably
0.004% or more.
Si: 0.1 to 1.0%
[0022] Si is an important element necessary for improving oxidation resistance. To ensure
oxidation resistance in exhaust gases at elevated temperatures, Si content needs to
be 0.1% or more. Meanwhile, excessive Si content beyond 1.0% deteriorates workability
at room temperature. Accordingly, the upper limit of Si content is set to 1.0%. Si
content is set to preferably 0.20% or more, more preferably 0.30% or more, and further
preferably 0.40% or more. Meanwhile, Si content is set to preferably 0.90% or less
and more preferably 0.60% or less.
Mn: 0.05 to 0.60%
[0023] Mn effectively improves thermal fatigue resistance due to improvement of spalling
resistance of oxide scale. To obtain such an effect, Mn content needs to be 0.05%
or more. Meanwhile, excessive Mn content beyond 0.60% deteriorates heat resistance
due to the formation of γ phase at a high temperature. Accordingly, Mn content is
set to 0.05% or more and 0.60% or less. Mn content is set to preferably 0.10% or more
and more preferably 0.15% or more. Meanwhile, Mn content is set to preferably 0.50%
or less and more preferably 0.40% or less.
P: 0.050% or less
[0024] P is a detrimental element that deteriorates toughness of steel and is thus desirably
reduced as much as possible. Accordingly, P content is set to 0.050% or less. P content
is preferably 0.040% or less, and more preferably 0.030% or less.
S: 0.008% or less
[0025] S reduces elongation and r-value, thereby adversely affecting formability. S is also
a harmful element that deteriorates corrosion resistance, which is the basic properties
of stainless steel, and is thus desirably reduced as much as possible. Accordingly,
in the present invention, S content is set to 0.008% or less. S content is preferably
0.006% or less.
Ni: 0.02 to 0.60%
[0026] Ni is an element that improves toughness and oxidation resistance of steel. To obtain
such an effect, Ni content is set to 0.02% or more. When oxidation resistance is insufficient,
thermal fatigue resistance deteriorates due to reduction in a cross-sectional area
of a material caused by an increased amount of oxide scale formed and/or spalling
of oxide scale. Meanwhile, Ni is a powerful γ phase-forming element. Accordingly,
excessive Ni content deteriorates oxidation resistance due to formation of γ phase
at a high temperature and deteriorates thermal fatigue resistance due to increase
in thermal expansion coefficient. Therefore, the upper limit of Ni content is set
to 0.60%. Ni content is preferably 0.05% or more and more preferably 0.10% or more.
Meanwhile, Ni content is preferably 0.40% or less and more preferably 0.30% or less.
Al: 0.001 to 0.25%
[0027] Al is an element that effectively improves oxidation resistance. To obtain such an
effect, Al content needs to be 0.001% or more. Meanwhile, Al is also an element that
increases a thermal expansion coefficient. A large thermal expansion coefficient results
in deterioration in thermal fatigue resistance. Moreover, considerable hardening of
steel deteriorates workability. Accordingly, Al content is set to 0.25% or less. Al
content is preferably 0.005% or more, more preferably more than 0.010%, and further
preferably more than 0.020%. Meanwhile, Al content is preferably less than 0.20% and
more preferably less than 0.08%.
Cr: 18.0 to 20.0%
[0028] Cr is an important element that effectively improves corrosion resistance and oxidation
resistance, which are the characteristics of stainless steel. However, when Cr content
is less than 18.0%, satisfactory oxidation resistance cannot be achieved in a high-temperature
range exceeding 900°C. When oxidation resistance is insufficient, the amount of oxide
scale formed increases and consequently, thermal fatigue resistance also deteriorates
due to reduction in a cross-sectional area of a material. Meanwhile, Cr is an element
that hardens steel and reduces ductility due to solid solution strengthening of steel
at room temperature. When Cr content exceeds 20.0%, the above-mentioned adverse effects
predominate and thermal fatigue resistance rather deteriorates. Accordingly, the upper
limit of Cr content is set to 20.0%. Preferably, Cr content is 18.5% or more. Meanwhile,
Cr content is preferably 19.5% or less.
Nb: 0.30 to 0.80%
[0029] Nb is an element important to the present invention for increasing high-temperature
strength, thereby improving thermal fatigue resistance and creep resistance. Such
an effect is obtained when Nb content is 0.30% or more. When Nb content is less than
0.30%, excellent thermal fatigue resistance or creep resistance cannot be obtained
due to insufficient strength at a high temperature. Meanwhile, when Nb content exceeds
0.80%, since a Laves phase (Fe
2Nb), which is an intermetallic compound, or the like tends to be precipitated, high-temperature
strength is decreased. Consequently, not only thermal fatigue resistance and creep
resistance deteriorate, but also embrittlement is promoted. Accordingly, Nb content
is set to 0.30% or more and 0.80% or less. Nb content is preferably 0.40% or more,
more preferably 0.45% or more, and further preferably more than 0.50%. Meanwhile,
Nb content is preferably 0.70% or less and more preferably 0.60% or less.
Mo: 1.80 to 2.50%
[0030] Mo is an effective element that improves thermal fatigue resistance and creep resistance
because it dissolves in steel and increase the high-temperature strength of steel.
Such an effect is realized when Mo content is 1.80% or more. When Mo content is less
than 1.80%, excellent thermal fatigue resistance or creep resistance cannot be obtained
due to insufficient high-temperature strength. Meanwhile, excessive Mo content not
only deteriorates workability due to hardening of steel, but also deteriorates thermal
fatigue resistance because Mo precipitates as a Laves phase (Fe
2Mo) in a similar manner to Nb and the amount of Mo dissolved in steel is reduced.
Moreover, Mo is precipitated, during a thermal fatigue test, since coarse σ phase
that acts as a starting point of fracture, thermal fatigue resistance deteriorates.
Accordingly, the upper limit of Mo content is set to 2.50%. Mo content is preferably
1.90% or more and more preferably more than 2.00%. Meanwhile, Mo content is preferably
2.30% or less and more preferably 2.10% or less.
N: 0.015% or less
[0031] N is an element that deteriorates toughness and formability of steel. When N content
exceeds 0.015%, not only toughness and formability deteriorate considerably, but also
creep resistance and thermal fatigue resistance deteriorate due to reduction in an
amount of dissolved Nb through formation of Nb nitride. Accordingly, N content is
set to 0.015% or less. From a viewpoint of ensuring toughness and formability, N is
preferably reduced as much as possible, and N content is desirably set to less than
0.010%.
Sb: 0.002 to 0.50%
[0032] Sb is an important element for improving creep resistance in the present invention.
Sb dissolves in steel and suppresses creep deformation of steel at a high temperature.
Without being precipitated as a carbonitride or a Laves phase even in a high-temperature
range, Sb remains dissolved in steel even after long-term use and suppresses creep
deformation, thereby making it possible to improve creep resistance. Such an effect
can be obtained when Sb content is 0.002% or more. Meanwhile, excessive Sb content
deteriorates toughness and hot workability of steel. Consequently, not only does cracking
readily occur during production, but also thermal fatigue resistance deteriorates
due to reduced hot ductility. Accordingly, the upper limit of Sb content is set to
0.50%. Sb content is preferably 0.005% or more and more preferably 0.020% or more.
Meanwhile, Sb content is preferably 0.30% or less and more preferably 0.10% or less.
Nb + Mo: 2.3 to 3.0% (1)
[0033] As in the foregoing, Nb and Mo are elements effective for improving thermal fatigue
resistance and creep resistance. Such effects are obtained when the respective contents
are 0.30% or more and 1.80% or more. However, to realize better thermal fatigue resistance
and better creep resistance than SUS444 in terms of a thermal fatigue life when the
temperature is elevated and lowered repeatedly between 200°C and 950°C to deal with
elevated exhaust gas temperatures, it is required to contain both elements within
the predetermined ranges and further to satisfy at least Nb + Mo ≥ 2.3%, in other
words, to set the amount of Nb + Mo (total content of Nb and Mo) to 2.3% or more.
When this condition is not satisfied, excellent creep resistance cannot be obtained
even when a predetermined amount of Sb is contained. Preferably, the condition is
Nb + Mo > 2.5%. Meanwhile, when the amount of Nb + Mo is excessively increased, excellent
thermal fatigue resistance and creep resistance are not achieved due to embrittlement
of steel. Accordingly, the upper limit of the mount of Nb + Mo is set to 3.0%. Preferably,
the amount of Nb + Mo is 2.7% or less.
[0034] Here, Nb and Mo in the above expression (1) represent the contents (mass%) of the
respective elements.
[0035] In the ferritic stainless steel of the present invention, the balance is Fe and inevitable
impurities.
[0036] The ferritic stainless steel of the present invention may further contain, in addition
to the above-described essential elements, one or two or more selected from Ti, Zr,
Co, B, V, W, Cu, and Sn as optional elements within the following ranges.
Ti: 0.01 to 0.16%
[0037] Ti is an element that improves corrosion resistance and formability, and prevents
intergranular corrosion of welds by stabilizing C and N. In the present invention,
Ti may be contained as necessary. If contained, Ti preferentially combines with C
and N compared with Nb. Consequently, it is possible to ensure the amount of Nb dissolved
in steel, which is effective for improving high-temperature strength. Moreover, heat
resistance is also effectively improved. Such effects can be obtained when Ti content
is 0.01% or more. Meanwhile, excessive Ti content beyond 0.16% causes deterioration
in toughness and adversely affects manufacturability, such as causing fracture through
repeated bending and unbending in a hot-rolled sheet annealing line. Moreover, Nb
carbonitride becomes readily precipitated by using Ti carbonitride as nuclei. Consequently,
the amount of Nb dissolved in steel, which is effective for improving high-temperature
strength, is rather reduced, thereby thermal fatigue resistance and creep resistance
deteriorate. Accordingly, if contained, Ti content is set to 0.01 to 0.16%. Ti content
is preferably 0.03% or more. Meanwhile, Ti content is preferably 0.12% or less, more
preferably 0.08% or less, and further preferably 0.05% or less.
Zr: 0.01 to 0.50%
[0038] Zr is an element that improves oxidation resistance. In the present invention, Zr
may be contained as necessary. The effect can be obtained when Zr content is 0.01%
or more. Meanwhile, when Zr content exceeds 0.50%, a Zr intermetallic compound is
precipitated, thereby embrittling steel. Accordingly, if contained, Zr content is
set to 0.01 to 0.50%. Zr content is preferably 0.03% or more and more preferably 0.05%
or more. Meanwhile, Zr content is preferably 0.30% or less and more preferably 0.10%
or less.
Co: 0.01 to 0.50%
[0039] Co is known as an element effective for improving toughness of steel. The effect
can be obtained when Co content is 0.01% or more. Meanwhile, since excessive Co content
rather deteriorates toughness of steel, the upper limit of Co content is set to 0.50%.
Accordingly, if contained, Co content is set to 0.01 to 0.50%. Co content is preferably
0.03% or more. Meanwhile, Co content is preferably 0.30% or less.
B: 0.0002 to 0.0050%
[0040] B is an element effective for improving workability, especially secondary workability,
of steel. Such an effect can be obtained when B content is 0.0002% or more. Meanwhile,
excessive B content deteriorates workability due to formation of BN. Accordingly,
if contained, B content is set to 0.0002 to 0.0050%. B content is preferably 0.0005%
or more and more preferably 0.0008% or more. Meanwhile, B content is 0.0030% or less
and more preferably 0.0020% or less.
V: 0.01 to 1.0%
[0041] V is an element effective for improving workability of steel as well as an element
effective for improving oxidation resistance. These effects are remarkable when V
content is 0.01% or more. Meanwhile, excessive V content beyond 1.0% deteriorates
not only toughness but also surface quality due to precipitation of coarse V(C, N).
Accordingly, if contained, V content is set to 0.01 to 1.0%. V content is preferably
0.03% or more and more preferably 0.05% or more. Meanwhile, V content is preferably
0.50% or less and more preferably 0.20% or less.
W: 0.01 to 5.0%
[0042] W is an element that significantly increases high-temperature strength through solid
solution strengthening in a similar manner to Mo. The effect can be obtained when
W content is 0.01% or more. Meanwhile, excessive W content not only hardens steel
considerably but also makes descaling during pickling difficult due to formation of
stable scale in an annealing step during production. Accordingly, if contained, W
content is set to 0.01 to 5.0%. Preferably, W content is 0.05% or more. Meanwhile,
W content is preferably 3.5% or less, more preferably 1.0% or less, and further preferably
less than 0.30%.
Cu: 0.01 to 0.40%
[0043] Cu is an element that effectively improves corrosion resistance of steel and is contained
when corrosion resistance is required. The effect can be obtained when Cu content
is 0.01% or more. Meanwhile, when Cu content exceeds 0.40%, oxide scale easily spalls
and cyclic oxidation resistance deteriorates. Accordingly, if contained, Cu content
is set to 0.01 to 0.40%. Cu content is preferably 0.03% or more and more preferably
0.06% or more. Meanwhile, Cu content is preferably 0.20% or less and more preferably
0.10% or less.
Sn: 0.001 to 0.005%
[0044] Sn is an element effective for increasing high-temperature strength of steel. The
effect can be obtained when Sn content is 0.001% or more. Meanwhile, excessive Sn
content rather deteriorates thermal fatigue resistance due to embrittlement of steel.
Accordingly, if contained, Sn content is set to 0.001 to 0.005%. Preferably, Sn content
is 0.001% or more and 0.003% or less.
[0045] The ferritic stainless steel of the present invention may further contain one or
two selected from Ca and Mg as optional elements within the following ranges.
Ca: 0.0002 to 0.0050%
[0046] Ca is an element effective for preventing clogging of nozzles that tend to occur
during continuous casting due to precipitation of Ti-based inclusions. The effect
can be obtained when Ca content is 0.0002% or more. Meanwhile, Ca content needs to
be 0.0050% or less in order to obtain good surface quality without forming surface
defects. Accordingly, if contained, Ca content is set to 0.0002 to 0.0050%. Ca content
is preferably 0.0005% or more. Meanwhile, Ca content is preferably 0.0030% or less
and more preferably 0.0020% or less.
Mg: 0.0002 to 0.0050%
[0047] Mg is an element effective for increasing the equiaxed crystal ratio of a slab and
improving workability and toughness. In a steel containing Nb and Ti as in the present
invention, Mg also effectively suppresses coarsening of Nb and/or Ti carbonitrides.
Such effects can be obtained when Mg content is 0.0002% or more. Coarsened Ti carbonitride
acts as a starting point of embrittlement cracking and thus considerably deteriorates
toughness. When Nb carbonitride coarsens, the amount of Nb dissolved in steel decreases,
thereby causing deterioration in thermal fatigue resistance. Meanwhile, when Mg content
exceeds 0.0050%, surface quality of steel deteriorates. Accordingly, if contained,
Mg content is set to 0.0002 to 0.0050%. Mg content is preferably 0.0003% or more and
more preferably 0.0004% or more. Meanwhile, Mg content is preferably 0.0030% or less
and more preferably 0.0020% or less.
[0048] The balance is Fe and inevitable impurities. When any of the above-described optional
elements is contained at less than the above-mentioned lower limit, such an optional
element is regarded as being contained as an inevitable impurity.
[0049] Next, a production method for a ferritic stainless steel of the present invention
will be described.
[0050] The production method for a ferritic stainless steel of the present invention may
suitably employ a common production method for a ferritic stainless steel and is not
particularly limited.
[0051] A ferritic stainless steel of the present invention can be produced, for example,
by a production process including: refining steel in a publicly known melting furnace,
such as a converter or an electric furnace; alternatively or additionally subjecting
to secondary refining, such as ladle refining or vacuum refining, to prepare steel
having the above-described chemical composition of the present invention; forming
into a slab by continuous casting or ingot casting and slabbing; and subsequently
forming into a cold-rolled annealed sheet through steps of hot rolling, hot-rolled
sheet annealing, pickling, cold rolling, finish annealing, pickling, and the like.
The above-mentioned cold rolling may be performed once or twice or more via intermediate
annealing. Moreover, each step of cold rolling, finish annealing, and pickling may
be performed repeatedly. Further, the hot-rolled sheet annealing may be omitted, and
when adjustment of the surface gloss or roughness of a steel sheet is required, skin-pass
rolling may be performed after cold rolling or finish annealing.
[0052] Preferable production conditions in the above-described production method will be
described.
[0053] In the steelmaking step for refining steel, steel melted in a converter, an electric
furnace, or the like is preferably subjected to secondary refining through the VOD
process, the AOD process, or the like to prepare steel containing the above-described
essential elements and optional elements added as necessary. The resulting refined
molten steel may be formed into a steel material by a publicly known method, but continuous
casting is preferably employed in view of productivity and quality. The steel material
is then heated to preferably 1,050°C to 1,250°C and hot rolled into a hot-rolled sheet
having a desirable thickness. From a production viewpoint, the thickness of the hot-rolled
sheet is desirably 5 mm or less. Naturally, it is also possible to form materials
other than sheets through hot working. The hot-rolled sheet is preferably formed into
a hot-rolled product by subjecting later, as necessary, to continuous annealing at
a temperature of 900°C to 1,150°C or batch annealing at a temperature of 700°C to
900°C, followed by descaling through pickling, polishing, or the like. Here, as necessary,
scale may be removed by shot blasting before pickling.
[0054] Further, the hot-rolled product (hot-rolled annealed sheet) may be formed into a
cold-rolled product through steps of cold rolling and so forth. In this case, cold
rolling may be performed once or twice or more via intermediate annealing in view
of productivity and/or required quality. The total reduction in cold rolling that
is performed once or twice or more is preferably 60% or more and more preferably 70%
or more. The cold-rolled steel sheet is preferably formed into a cold-rolled product
(cold-rolled annealed sheet) by subjecting later to continuous annealing (finish annealing)
at a temperature of preferably 900°C to 1,200°C and further preferably 1,000°C to
1,150°C, followed by pickling or polishing. Here, finish annealing may be performed
in a reducing atmosphere. In this case, pickling or polishing after finish annealing
may be omitted. Further, depending on uses, the shape, surface roughness, and/or material
properties of the steel sheet may be adjusted by subjecting to skin-pass rolling or
the like after finish annealing.
[0055] The hot-rolled product or cold-rolled product obtained as described above is later
subjected to processes, such as cutting, bending, bulging, and drawing, depending
on the respective uses and formed, for example, into an automotive or a motorcycle
exhaust pipe or converter case, an exhaust duct in a thermal power plant, or a fuel
cell-related component, such as a separator, an interconnector, or a reformer. Among
these uses, a ferritic stainless steel of the present invention is suitably used for
exhaust system components, such as exhaust manifolds, exhaust pipes, converter cases,
and mufflers. As one of its features, it is possible to obtain an exhaust manifold
with excellent durability, in particular, even when the temperature in use is elevated
to 700°C or higher by an exhaust gas from an engine.
[0056] A welding method for these components is not particularly limited and may employ
common arc welding, such as metal inert gas (MIG), metal active gas (MAG), or tungsten
inert gas (TIG) welding; electric resistance welding, such as spot welding or seam
welding; high-frequency resistance welding, such as electro-seam welding; high-frequency
induction welding, or the like.
EXAMPLES
[0057] Hereinafter, the present invention will be described in further detail by means of
Examples.
[0058] Each steel having any of the chemical compositions of No. 1 to 41, 43, and 45 to
47 shown in Table 1 was refined in a vacuum melting furnace, cast into a 50 kg-ingot,
heated at 1,170°C, and then hot-rolled into a 35 mm-thick sheet bar. The resulting
sheet bar was divided into two. One of the sheet bar was heated to 1,100°C, then hot-rolled
into a 5 mm-thick hot-rolled sheet, annealed in a temperature range of 1,000°C to
1,150°C, followed by grinding. Subsequently, the resulting hot-rolled annealed sheet
was cold rolled at a reduction of 70%, finish annealed at a temperature of 1,000°C
to 1,150°C, followed by descaling through pickling or polishing. The resulting 1.5
mm-thick cold-rolled annealed sheet was subjected to a creep test. As a reference,
a cold-rolled annealed sheet was also prepared from SUS444 (Conventional Example No.
28) in the same manner as described above and subjected to a creep test. The annealing
temperature was determined within the above-mentioned temperature ranges for each
steel under observation of the microstructure.
<Creep Test>
[0059] A specimen having the shape illustrated in Fig. 1 was cut out from each cold-rolled
annealed sheet obtained as described above and subjected to a creep test at 900°C
and an applied stress of 15 MPa. The specimen was evaluated as follows on the basis
of the time until rupture. The time until rupture was 5.5 hr for SUS444 (Conventional
Example No. 28), which was tested by way of comparison.
⊙: rupture time ≥ 10 hr
○: 6 hr ≤ rupture time < 10 hr
×: rupture time < 6 hr
[0060] In the above evaluation, ⊙ and ○ were regarded as acceptable and × as unacceptable.
The obtained results are shown in Table 1 (see creep at 900°C in Table 1).
[0061] Next, the other of the above-mentioned sheet bars after divided into two was heated
to 1,100°C and then hot forged into a 30 mm-square bar. Subsequently, the bar was
annealed at a temperature of 1,000°C to 1,150°C, then machined into a thermal fatigue
test specimen having the shape and dimension illustrated in Fig. 2, and subjected
to the following thermal fatigue test. The annealing temperature was set to a temperature
at which recrystallization is completed under observation of the microstructure for
every chemical composition. As a reference, a specimen was also prepared in the same
manner as described above for steel having the chemical composition of SUS444 (Conventional
Example No. 28) and subjected to the thermal fatigue test.
<Thermal Fatigue Test>
[0062] As illustrated in Fig. 3, a thermal fatigue test was performed under conditions that
elevate and lower the temperature repeatedly between 200°C and 950°C while restraining
the specimen at a restraint ratio of 0.5. On this occasion, the elevation rate of
the temperature was set to 5°C/s and the lowering rate of the temperature to 2°C/s.
Moreover, each holding time at 200°C and 950°C was set to 30 seconds. As illustrated
in Fig. 3, the above-mentioned restraint ratio can be represented as restraint ratio
η = a/(a + b), where a is (free thermal expansion strain - controlled strain)/2 and
b is (controlled strain)/2. Here, "free thermal expansion strain" means a strain when
the temperature is elevated without applying any mechanical stress, and "controlled
strain" means an absolute value of strain that is generated during the test. An actual
restraint strain that is generated in the material due to restraint is (free thermal
expansion strain - controlled strain).
[0063] Here, the thermal fatigue life was defined as the number of cycles when a stress
value is reduced to 75% of the stress value in an early cycle (fifth cycle in which
the test is stabilized), where the stress is calculated by dividing a load detected
at 200°C by the cross-sectional area of a uniformly heated parallel portion (see Fig.
2) of the specimen, and evaluated as follows. The thermal fatigue life was 650 cycles
for SUS444 (Conventional Example No. 28) tested by way of comparison.
⊙: 1,000 cycles or more (acceptable)
○: 800 cycles or more and less than 1,000 cycles (acceptable)
×: less than 800 cycles (unacceptable)
[0064] In the above evaluation, ⊙ and ○ were regarded as acceptable and × as unacceptable.
The obtained results are shown in Table 1 (see thermal fatigue life at 950°C in Table
1).
[Table 1]
| No. |
Chemical composition (mass%) |
Nb+Mo |
Creep at 900°C |
Thermal fatigue life at 950°C |
Note |
| C |
Si |
Mn |
P |
S |
Al |
Ni |
Cr |
Nb |
Mo |
Sb |
N |
Others |
| 1 |
0.005 |
0.44 |
0.59 |
0.032 |
0.001 |
0.031 |
0.25 |
19.6 |
0.57 |
2.08 |
0.036 |
0.006 |
|
2.65 |
○ |
○ |
Example |
| 2 |
0.004 |
0.78 |
0.13 |
0.027 |
0.002 |
0.170 |
0.19 |
19.9 |
0.51 |
2.03 |
0.038 |
0.005 |
Ti:0.13 |
2.54 |
⊙ |
⊙ |
Example |
| 3 |
0.004 |
0.22 |
0.08 |
0.025 |
0.002 |
0.089 |
0.11 |
18.8 |
0.35 |
2.50 |
0.070 |
0.005 |
|
2.85 |
○ |
○ |
Example |
| 4 |
0.005 |
0.55 |
0.30 |
0.030 |
0.002 |
0.005 |
0.26 |
19.8 |
0.60 |
2.03 |
0.072 |
0.006 |
Ti:0.04 |
2.62 |
○ |
○ |
Example |
| 5 |
0.005 |
0.71 |
0.15 |
0.029 |
0.002 |
0.087 |
0.30 |
18.4 |
0.53 |
2.10 |
0.080 |
0.005 |
Ti:0.15 |
2.63 |
○ |
○ |
Example |
| 6 |
0.006 |
0.62 |
0.24 |
0.020 |
0.001 |
0.080 |
0.12 |
19.8 |
0.67 |
2.00 |
0.066 |
0.007 |
|
2.67 |
○ |
○ |
Example |
| 7 |
0.004 |
0.60 |
0.49 |
0.036 |
0.003 |
0.088 |
0.55 |
19.5 |
0.50 |
2.09 |
0.037 |
0.006 |
|
2.59 |
○ |
○ |
Example |
| 8 |
0.004 |
0.92 |
0.17 |
0.026 |
0.003 |
0.047 |
0.16 |
18.1 |
0.47 |
1.95 |
0.057 |
0.005 |
|
2.42 |
○ |
○ |
Example |
| 9 |
0.006 |
0.44 |
0.34 |
0.027 |
0.002 |
0.083 |
0.13 |
18.6 |
0.58 |
2.15 |
0.054 |
0.006 |
|
2.73 |
⊙ |
⊙ |
Example |
| 10 |
0.005 |
0.30 |
0.13 |
0.025 |
0.002 |
0.082 |
0.07 |
18.7 |
0.55 |
2.07 |
0.320 |
0.007 |
|
2.62 |
⊙ |
⊙ |
Example |
| 11 |
0.004 |
0.31 |
0.16 |
0.029 |
0.002 |
0.020 |
0.28 |
19.1 |
0.56 |
2.00 |
0.020 |
0.007 |
|
2.56 |
○ |
○ |
Example |
| 12 |
0.005 |
0.62 |
0.18 |
0.030 |
0.003 |
0.022 |
0.19 |
18.2 |
0.54 |
1.97 |
0.024 |
0.006 |
Cu:0.34 |
2.51 |
○ |
○ |
Example |
| 13 |
0.004 |
0.32 |
0.19 |
0.028 |
0.001 |
0.023 |
0.14 |
18.8 |
0.50 |
2.00 |
0.085 |
0.005 |
Co:0.29 |
2.50 |
⊙ |
⊙ |
Example |
| 14 |
0.004 |
0.53 |
0.34 |
0.039 |
0.003 |
0.039 |
0.27 |
19.0 |
0.55 |
2.06 |
0.051 |
0.007 |
W:0.07 |
2.61 |
⊙ |
⊙ |
Example |
| 15 |
0.004 |
0.56 |
0.22 |
0.027 |
0.003 |
0.059 |
0.06 |
19.4 |
0.51 |
2.06 |
0.071 |
0.005 |
W:3.10 |
2.57 |
⊙ |
⊙ |
Example |
| 16 |
0.005 |
0.60 |
0.16 |
0.039 |
0.003 |
0.043 |
0.15 |
19.9 |
0.52 |
1.99 |
0.075 |
0.005 |
V:0.21 |
2.51 |
○ |
○ |
Example |
| 17 |
0.007 |
0.30 |
0.24 |
0.025 |
0.003 |
0.029 |
0.17 |
19.0 |
0.63 |
2.05 |
0.054 |
0.005 |
Zr:0.06 |
2.68 |
○ |
○ |
Example |
| 18 |
0.004 |
0.65 |
0.33 |
0.024 |
0.001 |
0.045 |
0.27 |
18.7 |
0.58 |
2.05 |
0.026 |
0.007 |
B:0.0009 |
2.63 |
○ |
○ |
Example |
| 19 |
0.006 |
021 |
0.28 |
0.028 |
0.002 |
0.090 |
0.18 |
19.6 |
0.56 |
1.88 |
0.039 |
0.008 |
Sn:0.003 |
2.44 |
○ |
○ |
Example |
| 20 |
0.004 |
0.39 |
0.38 |
0.029 |
0.001 |
0.034 |
0.29 |
18.2 |
0.57 |
2.01 |
0.054 |
0.006 |
Ca:0.0010 |
2.58 |
○ |
○ |
Example |
| 21 |
0.005 |
0.38 |
0.34 |
0.023 |
0.002 |
0.067 |
0.34 |
18.6 |
0.59 |
2.02 |
0.046 |
0.007 |
Mg:0.0011 |
2.61 |
○ |
○ |
Example |
| 22 |
0.005 |
0.78 |
0.25 |
0.036 |
0.003 |
0.065 |
0.30 |
19.2 |
0.53 |
1.99 |
0.041 |
0.005 |
Ca:0.0008, Mg:0.009 |
2.52 |
○ |
○ |
Example |
| 23 |
0.004 |
0.69 |
0.15 |
0.034 |
0.003 |
0.040 |
0.35 |
19.7 |
0.52 |
2.27 |
0.031 |
0.005 |
V:0.04, Cu:0.06 |
2.79 |
○ |
○ |
Example |
| 24 |
0.004 |
0.78 |
0.16 |
0.024 |
0.003 |
0.058 |
0.16 |
19.4 |
0.59 |
1.85 |
0.020 |
0.006 |
Co;0.03, V:0.06 |
2.44 |
○ |
○ |
Example |
| 25 |
0.004 |
0.30 |
0.18 |
0.028 |
0.001 |
0.081 |
0.08 |
19.9 |
0.51 |
2.46 |
0.074 |
0.005 |
Zr:0.08 |
2.97 |
○ |
○ |
Example |
| 26 |
0.007 |
0.45 |
0.37 |
0.032 |
0.001 |
0.066 |
0.07 |
19.2 |
0.60 |
1.81 |
0.093 |
0.005 |
B:0.0008, Ca:0.0006, Mg:0.0007 |
2.41 |
○ |
○ |
Example |
| 27 |
0.004 |
0.53 |
0.23 |
0.036 |
0.003 |
0.036 |
0.12 |
19.9 |
0.58 |
2.03 |
0.019 |
0.008 |
Co:0.02, B:0.0010, V:0.05, Cu:0.04, Ca:0.0007, Mg:0.0008 |
2.61 |
○ |
○ |
Example |
| 28 |
0.006 |
0.28 |
0.19 |
0.023 |
0.003 |
0.020 |
0.14 |
18.2 |
0.37 |
1.80 |
- |
0.008 |
|
2.17 |
× |
× |
Conventional Example SUS444 |
| 29 |
0.006 |
0.71 |
0.15 |
0.037 |
0.001 |
0.074 |
0.21 |
19.3 |
0.32 |
1.84 |
0.016 |
0.006 |
|
2.16 |
× |
× |
Comparative Example |
| 30 |
0.004 |
0.47 |
0.31 |
0.022 |
0.003 |
0.042 |
0.81 |
18.8 |
0.59 |
2.11 |
0.095 |
0.007 |
|
2.70 |
○ |
× |
Comparative Example |
| 31 |
0.007 |
0.45 |
0.19 |
0.027 |
0.003 |
0.072 |
0.22 |
16.8 |
0.48 |
2.00 |
0.086 |
0.005 |
|
2.48 |
○ |
× |
Comparative Example |
| 32 |
0.007 |
0.63 |
0.33 |
0.029 |
0.001 |
0.039 |
0.34 |
19.4 |
0.63 |
1.60 |
0.026 |
0.008 |
|
2.23 |
× |
× |
Comparative Example |
| 33 |
0.004 |
0.42 |
0.26 |
0.024 |
0.003 |
0.085 |
0.09 |
18.6 |
0.27 |
2.04 |
0.065 |
0.009 |
|
2.31 |
× |
× |
Comparative Example |
| 34 |
0.004 |
0.04 |
0.34 |
0.023 |
0.003 |
0.031 |
0.06 |
19.8 |
0.53 |
2.27 |
0.099 |
0.005 |
|
2.80 |
× |
× |
Comparative Example |
| 35 |
0.007 |
0.25 |
0.20 |
0.035 |
0.001 |
0.057 |
0.17 |
19.3 |
0.57 |
2.07 |
0.076 |
0.007 |
Ti:0.26 |
2.64 |
× |
× |
Comparative Example |
| 36 |
0.007 |
0.29 |
0.35 |
0.034 |
0.001 |
0.044 |
0.26 |
23.4 |
0.59 |
1.97 |
0.061 |
0.007 |
|
2.56 |
○ |
× |
Comparative Example |
| 37 |
0.005 |
0.72 |
0.02 |
0.037 |
0.001 |
0.049 |
0.10 |
18.3 |
0.56 |
2.06 |
0.026 |
0.006 |
|
2.62 |
○ |
× |
Comparative Example |
| 38 |
0.024 |
0.49 |
0.37 |
0.022 |
0.001 |
0.067 |
0.25 |
19.5 |
0.57 |
1.91 |
0.092 |
0.007 |
|
2.47 |
× |
× |
Comparative Example |
| 39 |
0.007 |
0.62 |
0.26 |
0.037 |
0.002 |
0.033 |
0.08 |
20.0 |
0.57 |
2.21 |
0.040 |
0.018 |
|
2.78 |
× |
× |
Comparative Example |
| 40 |
0.005 |
0.72 |
0.24 |
0.035 |
0.002 |
0.049 |
0.27 |
19.9 |
0.53 |
1.94 |
0.860 |
0.006 |
|
2.47 |
○ |
× |
Comparative Example |
| 41 |
0.005 |
0.23 |
0.17 |
0.025 |
0.002 |
0.062 |
0.08 |
18.0 |
0.60 |
2.80 |
0.088 |
0.007 |
|
3.40 |
× |
× |
Comparative Example |
| 43 |
0.007 |
0.39 |
0.20 |
0.036 |
0.002 |
0.033 |
0.22 |
18.2 |
0.50 |
1.91 |
0.016 |
0.005 |
Sn:0.06 |
2.41 |
○ |
× |
Comparative Example |
| 45 |
0.005 |
0.31 |
0.22 |
0.033 |
0.001 |
0.025 |
0.18 |
19.4 |
0.57 |
2.05 |
- |
0.008 |
|
2.62 |
× |
× |
Comparative Example |
| 46 |
0.005 |
0.47 |
0.15 |
0.030 |
0.002 |
0.039 |
0.29 |
18.9 |
0.91 |
1.98 |
0.042 |
0.007 |
|
2.89 |
× |
× |
Comparative Example |
| 47 |
0.006 |
0.56 |
0.31 |
0.029 |
0.002 |
0.044 |
0.22 |
19.1 |
0.77 |
2.47 |
0.051 |
0.008 |
|
3.24 |
× |
× |
Comparative Example |
| Note: Underlines indicate the outside of the scope of the present invention. |
[0065] As shown in Table 1, all the ferritic stainless steels of Examples No. 1 to 27 (hereinafter,
ferritic stainless steel is simply referred to as steel) exhibit better properties
than SUS444 (Conventional Example No. 28) in the creep test and the thermal fatigue
test.
[0066] In No. 29 steel having Nb + Mo content of less than 2.3 mass%, creep rupture time
and thermal fatigue life were unacceptable. In No. 30 steel having Ni content of more
than 0.60 mass%, thermal fatigue life was unacceptable. In No. 31 steel having Cr
content of less than 18.0 mass%, thermal fatigue life was unacceptable. In No. 32
steel having Mo content of less than 1.80 mass%, creep rupture time and thermal fatigue
life were unacceptable. In No. 33 steel having Nb content of less than 0.30 mass%,
both creep rupture time and thermal fatigue life were unacceptable. In No. 34 steel
having Si content of less than 0.1 mass%, oxidation was noticeably observed in both
the creep test and the thermal fatigue test, and both creep rupture time and thermal
fatigue life were unacceptable. In No. 35 steel having Ti content of more than 0.16
mass%, both creep rupture time and thermal fatigue life were unacceptable. In No.
36 steel having Cr content of more than 20.0 mass%, thermal fatigue life was unacceptable
due to embrittlement of steel. In No. 37 steel having Mn content of less than 0.05
mass%, spalling of oxide scale occurred during the thermal fatigue test and thermal
fatigue life was unacceptable. In No. 38 steel having C content of more than 0.020
mass%, both creep rupture time and thermal fatigue life were unacceptable due to a
reduced amount of Nb in steel. In No. 39 steel having N content of more than 0.015
mass%, creep rupture time and thermal fatigue life were unacceptable due to a reduced
amount of Nb in steel by precipitation of Nb nitride. In No. 40 steel having Sb content
of more than 0.50 mass%, thermal fatigue life was unacceptable due to reduced hot
ductility. In No. 41 steel having Mo content of more than 2.50 mass%, coarse σ phase
(Fe-Cr-based intermetallic compound) precipitated during the thermal fatigue test
and consequently, thermal fatigue life was unacceptable. In addition, creep rupture
time was also unacceptable. In No. 43 steel having Sn content of more than 0.005 mass%,
thermal fatigue life was unacceptable. In No. 45 steel without Sb, both creep rupture
time and thermal fatigue life were unacceptable. In No. 46 steel having Nb content
of more than 0.80 mass%, both creep rupture time and thermal fatigue life were unacceptable.
In No. 47 steel having Nb + Mo content of more than 3.0%, both creep rupture time
and thermal fatigue life were unacceptable.
Industrial Applicability
[0067] A ferritic stainless steel of the present invention is not only suitable for exhaust
system components of automobiles and so forth but also well usable for exhaust system
components in thermal power generation systems and for solid oxide fuel cell components,
for both of which similar properties are required.