FIELD OF INVENTION
[0001] The present invention relates to maraging steels.
BACKGROUND OF INVENTION
[0002] Gas turbines and steam turbines for use in thermal power facilities each include
a rotor and blades, where the rotor acts as a rotating shaft. The rotor functionally
supports the blades and transmits turning force (torque) to a generator. The rotor,
as to be exposed to a high-temperature environment at about 500°C, is made of any
of heat-resisting materials. Such heat-resisting materials are mainly selected from
ferritic heat-resisting steels and Ni-based alloys.
[0003] Exemplary practically used ferritic heat-resisting steels for rotors are high-chromium
ferritic steels such as 12%-Cr steels. The high-chromium ferritic steels, however,
are significantly inferior in strength at high temperatures (high-temperature strength)
to Ni-based alloys, which are expensive. Austenitic stainless steels, which are widely
used as general heat-resisting materials, are not suitable as materials for rotors,
which are large-scale members. This is because the austenitic stainless steels have
high coefficients of thermal expansion, although they have high-temperature strength
lying midway between that of the ferritic heat-resisting steels and that of the Ni-based
alloys. In addition to these materials, exemplary known heat-resisting materials for
rotors include precipitation-hardened iron-based high heat-resistance alloys (superalloys)
such as "A286", and precipitation-hardened ferritic heat-resisting steels such as
maraging steels.
[0004] Of these heat-resisting materials, the maraging steels are materials strengthened
(hardened) by aging precipitation of martensitic phases and intermetallic compounds
and are produced via quenching and aging heat treatments. The maraging steels are
significantly superior in high-temperature strength to ferritic heat-resisting steels.
Disadvantageously, however, the maraging steels have lower toughness when designed
to have such a chemical composition and to be subjected to a heat treatment under
such conditions as to offer high strength at high temperatures. In particular, steels
for rotors of gas turbines and steam turbines for use in thermal power facilities
require excellent toughness, because high heat stress is generated when the temperatures
of the steels fall down to room temperature during suspension of operation.
[0005] There have been proposed various techniques so as to improve both strength and toughness.
For example, Japanese Patent No.
5362995 proposes a stainless steel alloy including, by weight: 0.002% to 0.015% carbon (C),
2% to 15% cobalt (Co), 7.0% to 14.0% nickel (Ni), 8.0% to 15.0% chromium (Cr), 0.5%
to 2.6% molybdenum (Mo), 0.4% to 0.75% titanium (Ti), less than 0.5% tungsten (W),
less than 0.7% aluminum (Al), with the balance essentially iron (Fe) and incidental
elements and impurities. The alloy avoids copper (Cu) as an alloying constituent,
has a lath martensite microstructure having undergone predetermined treatments, and
has a volume fraction of retained austenite of less than 15%, essentially without
topologically close packed (TCP) intermetallic phases. In the alloy, the carbon (C)
is in a dispersion of 0.02% to 0.15% by volume TiC carbide particles. The alloy further
includes a dispersion of intermetallic particles primarily of Ni
3Tiη phase as a strengthening phase.
[0006] Japanese Unexamined Patent Application Publication (
JP-A) No. 2015-61932 proposes a maraging steel excellent in fatigue characteristics. The maraging steel
has a chemical composition including, in mass percent: C in a content of 0.015% or
less, Ni in a content of 12.0% to 20.0%, Mo in a content of 3.0% to 6.0%, Co in a
content of 5.0% to 13.0%, Al in a content of 0.01% to 0.3%, Ti in a content of 0.2%
to 2.0%, O in a content of 0.0020% or less, N in a content of 0.0020% or less, and
Zr in a content of 0.001% to 0.02%, with the balance being Fe and unavoidable impurities.
[0007] JP-A No. Hei04(1992)-59922 proposes a method for producing a maraging steel. The method includes subjecting
a maraging steel to a recrystallization solution treatment, an unrecrystallized solution
treatment, and an aging heat treatment. The maraging steel contains, in mass percent,
C in a content of 0.05% or less, Si in a content of 0.2% or less, Mn in a content
of 0.2% or less, P in a content of 0.05% or less, S in a content of 0.05% or less,
Ni in a content of 10.0% to 21.0%, Co in a content of 9.5% to 15.0%, Mo in a content
of 3.0% to 12.0%, Ti in a content of 0.2% to 1.6%, Al in a content of 0.30% or less,
and B in a content of 0.0005% to 0.0020%, and the maraging steel has undergone hot
forming. In the method, the recrystallization solution treatment is performed as a
two-stage treatment including heating in a temperature range of from 1000°C to 1180°C
for one minute or longer, cooling at a cooling rate of 20°C/min or more, and further
heating in a temperature range of from 800°C to 950°C for one minute or longer, and
then cooling.
SUMMARY OF INVENTION
[0008] The technique described in Japanese Patent No.
5362995 allows a stainless steel alloy to have higher strength and better toughness by adjusting
the chemical composition and microstructure of the alloy. The technique evaluates
strength and room-temperature toughness, but fails to evaluate strength at high temperatures
of about 500°C, to which high temperatures the present invention is to be applied.
[0009] The technique described in
JP-A No. 2015-61932 offers excellent fatigue strength by refinement of TiN inclusions, but fails to evaluate
strength at high temperatures of about 500°C, to which high temperatures the present
invention is to be applied. Maraging steels offer more excellent high-temperature
strength as compared with ferritic heat-resisting steels. The maraging steels, however,
do not always maintain such excellent high-temperature strength as intact when controlled
to have higher fatigue strength and better toughness.
[0010] JP-A No. Hei04(1992)-59922 mentions that a maraging steel having strength, toughness, and ductility at better
levels is obtained by appropriately controlling the heat treatment conditions. However,
the technique described in this literature also fails to evaluate strength at high
temperatures to which the present invention is to be applied, as with the technique
described in Japanese Patent No.
5362995 and
JP-A No. 2015-61932.
[0011] The present invention has been made under these circumstances and has an object to
improve the toughness of a maraging steel which is more inexpensive as compared with
Ni-based alloys and has higher strength at high temperatures as compared with ferritic
heat-resisting steels and to provide a maraging steel having high-temperature strength
and room-temperature toughness both at excellent levels.
[0012] The present invention has achieved the object and provides, in an embodiment, a maraging
steel containing, in combination, in mass percent, C in a content from greater than
0% to 0.02%, Mn in a content from greater than 0% to 0.3%, Si in a content from greater
than 0% to 0.3%, Ni in a content of 10% to 13%, Mo in a content of 0.5% to 3.5%, Co
in a content of 9% to 12%, Cr in a content of 1.5% to 4.5%, Ti in a content of 1.5%
to 4.5%, and Al in a content of 0.01% to 0.2%, with the remainder consisting of iron
and inevitable impurities. In the maraging steel, the total content of the Ti and
Mo is 5.0% or less, and the ratio ([Mo]/[Ti]) of the Mo content [Mo] to the Ti content
[Ti] is 1.0 or less.
[0013] The maraging steel according to the present invention preferably has a phosphorus
(P) content from greater than 0% to 0.01%, a nitrogen (N) content from greater than
0% to 0.01%, and a sulfur (S) content from greater than 0% to 0.01%, where P, N, and
S are present in the inevitable impurities. The maraging steel preferably has a surface
hardness in terms of Vickers hardness of 400 Hv or more.
[0014] The present invention can actually provide a maraging steel which not only has excellent
high-temperature strength by aging precipitation of intermetallic compounds, but also
offers good room-temperature toughness by controlling the chemical composition and
microstructure. The maraging steel as above offers excellent high-temperature strength
and good room-temperature toughness and is very useful typically as materials for
rotors for use in thermal power facilities. The maraging steel, when applied to materials
for rotors for use in thermal power facilities, gives rotors which are inexpensive
and still have lighter weights as compared with conventional Ni-based alloy rotors,
and can contribute to improved generation efficiency and thereby to CO
2 emission control.
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS
[0015] The inventors of the present invention made investigations from various different
angles so as to actually provide a maraging steel which features compatibility between
high-temperature strength and room-temperature toughness. In particular, to achieve
the high-temperature strength, the inventors made intensive investigations on how
the chemical composition and the microstructure state determined by aging heat treatment
after quenching effect the room-temperature toughness.
[0016] In regular maraging steels, precipitates to perform precipitation strengthening are
generally intermetallic compounds mainly containing Mo. Assume that a maraging steel
has such a chemical composition as to tend to form such intermetallic compounds. In
this maraging steel, a Laves phase including Fe
2Mo, which is a binary intermetallic compound, tends to form upon aging heat treatment
of the maraging steeL The maraging steel, when containing a larger amount of the Laves
phase, tends to readily have lower toughness. In particular, the aging heat treatment
of materials to form rotors, which are large-sized members, is performed at a high
temperature for a long time, and thereby causes the compound to be readily formed
in a large amount, and this lowers the toughness.
[0017] The inventors then hit on an idea that conversion of the intermetallic compounds
mainly containing Mo into such intermetallic compounds as not to adversely affect
toughness may actually provide good toughness without occurrence of the above-mentioned
problems. After further investigations, the inventors found such a chemical composition
as to form intermetallic compounds mainly including Ti, such as Ni
3Ti intermetallic compound. The present invention has been made on the basis of these
findings.
[0018] A maraging steel having the chemical composition specified in the present invention,
when subjected to an aging heat treatment under predetermined conditions, has a microstructure
in which finely divided martensite is dispersed in a ferritic phase in which the Ni
3Ti intermetallic compound is precipitated. This maraging steel offers such properties
as to offer a surface hardness in terms of Vickers hardness of 400 Hv or more.
[0019] As apparent from the above-mentioned concept, appropriate settings of: among the
chemical composition, in particular the Mo and Ti contents and the relationship between
them are important in the maraging steel according to the present invention. Conversion
into the precipitates of intermetallic compounds as above requires appropriate settings
of not only the contents of Mo and Ti and the total contents of them, but also the
ratio ([Mo]/[Ti]) of the Mo content [Mo] to the Ti content [Ti]. Reasons for the settings
of these factors are as follows.
Mo: 0.5% to 3.5%, Ti: 1.5% to 4.5%
[0020] Molybdenum (Mo) and titanium (Ti) form precipitates of various intermetallic compounds
mainly containing these elements and are useful for higher strength and better toughness
of the steel. To offer these advantageous effects effectively, the steel is controlled
to contain Mo in a content of 0.5% or more and Ti in a content of 1.5% or more, and
preferably contains Mo in a content of 1.0% or more and Ti in a content of 2.0% or
more.
[0021] However, the steel, if having an excessively high Mo content, may suffer from the
formation of a larger amount of Fe
2Mo, which adversely affects toughness. To eliminate or minimize this, the Mo content
is controlled to 3.5% or less, preferably 3.0% or less, and more preferably 2.5% or
less. The steel, if having an excessively high Ti content, may suffer from insufficient
room-temperature durability. To eliminate or minimize this, the Ti content is controlled
to 4.5% or less, preferably 4.0% or less, and more preferably 3.5% or less.
[0022] Total Content of Mo and Ti: 5.0% or less, Ratio ([Mo]/[Ti]): 1.0 or less
[0023] In addition to the settings of the Mo and Ti contents as above, providing of intermetallic
compounds formed in the steel mainly including not Mo, but Ti requires the control
of the total content of Mo and Ti to 5.0% or less, and the control of the ratio ([Mo]/[Ti])
to 1.0 or less.
[0024] Increase or decrease of the total content of Mo and Ti causes toughness and high-temperature
strength to vary in a trade-off manner. To keep toughness and high-temperature strength
in balance, the total content of Mo and Ti is controlled to 5.0% or less. The steel,
if having a total content of Mo and Ti of greater than 5.0%, has satisfactory high-temperature
strength, but fails to surely have toughness, because of excessive amounts of precipitated
various intermetallic compounds. The total content is preferably 4.0% or less, and
more preferably 3.0% or less. The total content in terms of lower limit is inevitably
2.0% or more on the basis of the contents of the respective elements, but is preferably
2.2% or more.
[0025] In contrast, the steel, if having a ratio ([Mo]/[Ti]) (namely, mass ratio) of the
Mo content [Mo] to the Ti content [Ti] of greater than 1.0, fails to surely have toughness,
because of a larger proportion of the Laves phase. The ratio ([Mo]/[Ti]) is preferably
0.8 or less, and more preferably 0.6 or less. The ratio ([Mo]/[Ti]) in terms of lower
limit is 0.11 or more on the basis of the respective contents, but is preferably 0.2
or more, and more preferably 0.3 or more.
[0026] The settings of the total content of Mo and Ti and the ratio ([Mo]/[Ti]) of the Mo
content [Mo] to the Ti content [Ti] within the predetermined ranges allows the steel
to have toughness and high-temperature strength both at satisfactory levels. However,
the aging heat treatment, if performed at an excessively high temperature and/or for
an excessively long time, may fail to give sufficient high-temperature strength. To
eliminate or minimize this, the temperature and time conditions in the aging are preferably
controlled so as to allow the steel to have a surface Vickers hardness of 400 Hv or
more, as mentioned below.
[0027] In the maraging steel according to the present invention, at least Mo and Ti are
to be controlled as mentioned above, but, in addition to these elements, elements
such as C, Mn, Si, Ni, Co, Cr, and Al are to be controlled within appropriate ranges.
Reasons for the settings on these elements are as follows.
C: from greater than 0% to 0.02%
[0028] Carbon (C) forms carbides in a high-temperature environment to allow the steel to
have high-temperature strength and high-temperature creep strength at higher levels.
However, the carbon content should be minimized so as to maximize the precipitation
of intermetallic compounds mainly containing Ti. The steel, if having an excessively
high carbon content of greater than 0.02%, may contrarily have lower toughness because
of formation of TiC in a larger amount. The carbon content in terms of upper limit
is preferably 0.015% or less, and more preferably 0.010% or less. The carbon content
in terms of lower limit is preferably 0.001% or more, and more preferably 0.005% or
more, so as to allow carbon to offer basic actions.
Mn: from greater than 0% to 0.3%
[0029] Manganese (Mn) has a deoxidation action in molten steel. The element offers the advantageous
effect more with an increasing content of the element. To offer the advantageous effect
effectively, the Mn content is preferably controlled to 0.005% or more. The Mn content
in terms of lower limit is more preferably 0.010% or more, and furthermore preferably
0.015% or more. However, the steel, if having an excessively high Mn content of greater
than 0.3%, may fail to include the martensitic phase after quenching, due to increased
stability of the austenitic phase. The Mn content in terms of upper limit is preferably
0.2% or less, and more preferably 0.1% or less.
Si: from greater than 0% to 0.3%
[0030] Silicon (Si) has a deoxidation action in molten steel, as with Mn. This element,
even when present in a trace amount, effectively allows the steel to have better oxidation
resistance. To offer these advantageous effects effectively, the Si content is preferably
controlled to 0.005% or more. The Si content in terms of lower limit is preferably
0.010% or more, and furthermore preferably 0.015% or more. However, the steel, if
having an excessively high Si content, may suffer from impaired ductility because
of excessive work hardening. To eliminate or minimize this, the Si content is controlled
to 0.3% or less. The Si content in terms of upper limit is preferably 0.2% or less,
and more preferably 0.1% or less.
Ni: 10% to 13%
[0031] Nickel (Ni) is an austenitic phase-stabilizing element which is necessary for austenitization
of the microstructure in heating before quenching. This element also allows Ti to
be precipitated as the Ni
3Ti intermetallic compound and thereby allows the steel to have more satisfactory high-temperature
strength. To offer these advantageous effects, the Ni content is controlled to 10%
or more. The Ni content is preferably 10.5% or more, and more preferably 11.0% or
more. However, the steel, if having an excessively high Ni content of greater than
13%, may cause higher cost and may cause austenite to remain after quenching. The
Ni content in terms of upper limit is preferably 12.5% or less, and more preferably
12.0% or less.
Co: 9% to 12%
[0032] Cobalt (Co) is dissolved as a solute in the steel to offer solid-solution strengthening.
To offer the advantageous effect, the Co content is controlled 9% or more. The Co
content in terms of lower limit is preferably 9.5% or more, and more preferably 10.0%
or more. However, the steel, if having an excessively high Co content, may cause higher
cost and may have impaired ductility due to excessively increased strength. To eliminate
or minimize these, the Co content in terms of upper limit is controlled to 12% or
less, and is preferably 11.5% or less, and more preferably 11.0% or less.
Cr: 1.5% to 4.5%
[0033] Chromium (Cr) is necessary for better oxidation resistance of the maraging steel.
To offer good oxidation resistance, the Cr content is controlled to 1.5% or more.
The Cr content in terms of lower limit is preferably 2.0% or more, and more preferably
2.5% or more. However, the steel, if having an excessively high Cr content, may be
embrittled due to the formation of σ phases in a high-temperature environment in which
the steel is used as a product. To eliminate or minimize this, the Cr content in terms
of upper limit is controlled to 4.5% or less, and is preferably 4.0% or less, and
more preferably 3.5% or less.
Al: 0.01% to 0.2%
[0034] Aluminum (Al) has a deoxidation action in molten steel, as with Mn. To offer the
advantageous effect, the Al content is controlled to 0.01% or more. The Al content
in terms of lower limit is preferably 0.02% or more, and more preferably 0.03% or
more. However, the steel, if having an excessively high Al content, may suffer from
formation of coarse inclusions derived from Al. To eliminate or minimize this, the
Al content is controlled to 0.2% or less, and is preferably 0.1% or less, and more
preferably 0.05% or less.
[0035] The chemical composition specified in the present invention is as described above,
with the remainder being iron and inevitable impurities. Of the inevitable impurities,
P, N, and S are preferably decreased to levels as mentioned below. The impurities
excluding P, N, and S may include low-melting-point impurity metals derived from scrap
raw materials, such as Sn, Pb, Sb, As, and Zn. These elements, however, lower grain-boundary
strength during hot working and in use in a high-temperature environment and are desirably
minimized, in content.
P: from greater than 0% to 0.01%
[0036] Phosphorus (P) is an inevitably-contaminated impurity, and causes the steel to have
lower weldability with an increasing content thereof. From this viewpoint, phosphorus
is preferably minimized, and the phosphorus content is controlled to preferably 0.01%
or less, more preferably 0.005% or less, and furthermore preferably 0.001% or less.
N: from greater than 0% to 0.01%
[0037] Nitrogen (N) is also an inevitably-contaminated impurity, fixes Ti as nitrides, and
lowers the amounts of formed intermetallic compounds that contribute to higher strength,
where Ti is contained as an essential element in the steel according to the present
invention. From this viewpoint, nitrogen is preferably minimized, and the nitrogen
content is controlled to preferably 0.01% or less, more preferably 0.005% or less,
and furthermore preferably 0.001% or less.
S: from greater than 0% to 0.01%
[0038] Sulfur (S) is also an inevitably-contaminated impurity and impairs hot workability
necessary typically for forging, with an increasing content thereof From this viewpoint,
sulfur is preferably minimized, and the sulfur content is controlled to preferably
0.01% or less, more preferably 0.005% or less, and furthermore preferably 0.001% or
less.
[0039] The maraging steel according to the present invention has a chemical composition
as mentioned above. The steel having the chemical composition can be easily obtained
by adjusting proportions of raw materials as appropriate via melting. Ingots obtained
by ingot making may be subjected to homogenization or soaking (hereinafter also referred
to "soaking treatment") as needed, subjected to hot working to adjust its shape, and
then subjected to an appropriate quenching heat treatment and a subsequent aging heat
treatment.
[0040] When the ingots are those obtained by ingot making, the soaking treatment eliminates
or minimizes solidifying segregation of the ingots, by holding the ingots in a temperature
range of typically from 1250°C to 1300°C for about 10 hours. The hot working may be
performed while heating the work at a temperature of about 1000°C or higher.
[0041] The steel obtained by subjecting an ingot to the soaking treatment and hot working
is subjected to quenching so as to form a martensitic phase. The heating temperature
in quenching, namely, the heating temperature before cooling is controlled within
such a temperature range that the entire steel becomes an austenitic phase and that
precipitates undergo solutionization. The steel according to the present invention
having the chemical composition as above is preferably subjected to quenching performed
at a heating temperature of 900°C or higher, more preferably 950°C or higher, and
furthermore preferably 1000°C or higher. However, quenching, if performed at an excessively
high heating temperature, may cause the austenitic phase to coarsen, and this may
impede the formation of finely divided martensite. From this viewpoint, the heating
temperature in quenching is controlled to preferably 1150°C or lower, more preferably
1100°C or lower, and furthermore preferably 1050°C or lower.
[0042] Cooling in quenching is preferably performed via air cooling or water cooling. Cooling
in a temperature range down to 80°C, which is lower than the martensitic transformation
start temperature Ms, is preferably performed at a cooling rate of 5°C/hr or more.
The cooling rate in this temperature range is more preferably 10°C/hr or more, and
furthermore preferably 20°C/hr or more. However, the cooling rate has a ceiling with
respect to such large-sized steels and is about 100°C/hr or less.
[0043] The steel, in which the martensitic phase is formed in the above manner, has very
high strength, but has low ductility and toughness, and thus requires an aging heat
treatment so as to adjust balance between strength and toughness, where the aging
heat treatment corresponds to a tempering heat treatment.
[0044] The aging heat treatment is performed in such a temperature range as not to increase
the austenitic phase, namely, at a temperature lower than the Ac
3 transformation temperature. For the maraging steel having the chemical composition
as above, the upper limit temperature is 675°C. Accordingly, the temperature and holding
time of the aging heat treatment are controlled in a temperature range lower than
675°C so that the steel has a surface Vickers hardness of 400 Hv or more.
[0045] The aging heat treatment is not limited in temperature and holding time, except for
the temperature upper limit. However, the aging heat treatment, typically when performed
at a set temperature of 650°C, can stably give a sufficient hardness when performed
for a holding time of 3 hours or shorter. To allow the aging heat treatment to proceed
effectively at that temperature, the holding time is preferably at least one hour
or longer, and is more preferably 1.5 hours or longer.
[0046] The present invention will be illustrated in further detail on operation and advantageous
effects thereof with reference to several examples below. It should be noted, however,
that the examples are by no means intended to limit the scope of the present invention;
and that various modifications and changes in design without deviating from the spirit
and scope of the present invention described herein all fall within the technical
scope of the present invention.
Examples
[0047] Steels A to I having chemical compositions given in Table 1 were heated and melted
using a vacuum induction furnace, cast into 20-kg ingots, subjected to a soaking treatment
at 1280°C for 12 hours, and further subjected to hot forging to be processed into
steels having a size of 60 mm in width by 15 mm thickness by L in length.
[Table 1]
Steel |
Chemical composition* (in mass percent) |
C |
Si |
Mn |
P |
S |
Ni |
Cr |
Co |
Mo |
Ti |
Al |
N |
A |
0.009 |
0.018 |
0.009 |
0.005 |
0.001 |
11.9 |
3.1 |
9.8 |
1.9 |
2.0 |
0.07 |
0.001 |
B |
0.006 |
0.008 |
0.010 |
0.004 |
0.001 |
12.0 |
3.1 |
9.8 |
1.0 |
2.0 |
0.09 |
0.001 |
C |
0.015 |
0.056 |
0.130 |
0.008 |
0.001 |
11.3 |
2.2 |
11.3 |
2.0 |
2.8 |
0.05 |
0.008 |
D |
0.012 |
0.182 |
0.094 |
0.003 |
0.001 |
11.6 |
2.5 |
10.3 |
0.8 |
2.3 |
0.06 |
0.003 |
E |
0.008 |
0.087 |
0.209 |
0.009 |
0.001 |
12.1 |
2.7 |
10.8 |
2.4 |
2.5 |
0.04 |
0.002 |
F |
0.014 |
0.116 |
0.165 |
0.004 |
0.002 |
10.8 |
2.9 |
9.9 |
1.9 |
2.6 |
0.05 |
0.005 |
G |
0.011 |
0.143 |
0.055 |
0.005 |
0.001 |
11.0 |
2.8 |
10.1 |
3.0 |
1.7 |
0.04 |
0.003 |
H |
0.013 |
0.221 |
0.245 |
0.007 |
0.001 |
10.5 |
3.4 |
11.0 |
1.6 |
4.2 |
0.02 |
0.008 |
I |
0.003 |
0.014 |
0.012 |
0.002 |
0.001 |
12.1 |
3.0 |
10.3 |
5.0 |
2.0 |
0.10 |
0.002 |
* Remainder: iron and inevitable impurities excluding P, S, and N |
[0048] The obtained steels were heated at 1000°C for 15 minutes, subjected to quenching
via water-immersion cooling, and each subjected to an aging heat treatment in a temperature
range of from 650°C to 700°C for a time range of from 2 to 30 hours, under one of
four conditions (a), (b), (c), and (d) as follows.
[0049] Aging Heat Treatment Conditions
- (a) At a temperature of 650°C for a holding time of 3 hours
- (b) At a temperature of 650°C for a holding time of 30 hours
- (c) At a temperature of 700°C for a holding time of 30 hours
- (d) At a temperature of 650°C for a holding time of 2 hours
[0050] Table 2 presents the steel type and the aging heat treatment condition each employed
in Tests Nos. 1 to 12, together with the total content of Mo and Ti, and the ratio
([Mo]/[Ti]).
[Table 2]
Test number |
Steel |
Total content (in mass percent) of Mo and Ti |
Ratio ([Mo]/[Ti]) |
Aging heat treatment condition |
1 |
A |
3.9 |
0.95 |
(a) |
2 |
B |
3.0 |
0.50 |
(a) |
3 |
B |
3.0 |
0.50 |
(d) |
4 |
C |
4.8 |
0.71 |
(a) |
5 |
D |
3.1 |
0.35 |
(a) |
6 |
E |
4.9 |
0.96 |
(a) |
7 |
F |
4.5 |
0.73 |
(a) |
8 |
G |
4.7 |
1.76 |
(a) |
9 |
H |
5.8 |
0.38 |
(a) |
10 |
I |
7.0 |
2.50 |
(a) |
11 |
I |
7.0 |
2.50 |
(b) |
12 |
I |
7.0 |
2.50 |
(c) |
[0051] From the above-prepared steels, flanged round bar test specimens each including a
gauge portion of 6 mm in diameter by 30 mm in length were prepared, subjected to high-temperature
tensile tests at 500°C in accordance with the method prescribed in Japanese Industrial
Standard (JIS) G 0567:2012, to determine a 0.2% yield strength as a high-temperature
strength. A sample, when having a 0.2% yield strength as measured of 750 MPa or more,
is judged to surely have excellent high-temperature strength.
[0052] From the above-prepared steels, full-size 2-mmV notch Charpy test specimens in conformity
with JIS Z 2242:2005 were prepared, subjected to Charpy impact tests to measure Charpy
impact values at 0°C, on the basis of which toughness was evaluated. The present invention
is to improve toughness at room temperature of about 25°C. A sample, when having good
toughness at 0°C, can be judged to also have good toughness at room temperature. On
the basis of these, toughness was evaluated at 0°C. A sample, when having a Charpy
impact value as measured of 10.0 J/cm
2 or more, can be judged to offer more excellent toughness as compared with conventional
maraging steels. The Charpy impact value is preferably 15.0 J/cm
2 or more, and more preferably 17.0 J/cm
2 or more.
[0053] The above-prepared steels, namely, steels after the aging heat treatment, were subjected
to mirror-like finishing via mechanical polishing, followed by measurements of surface
Vickers hardness at a load of 500 g. A sample steel, when having a surface Vickers
hardness of 400 Hv or more, can be judged to have excellent surface hardness.
[0054] Evaluation results on the high-temperature strength, Charpy impact value, and Vickers
hardness are presented in Table 3.
[Table 3]
Test number |
High-temperature strength (MPa) |
Charpy impact value (J/cm2) |
Vickers hardness (Hv) |
1 |
835 |
12.3 |
443 |
2 |
781 |
17.6 |
430 |
3 |
847 |
15.8 |
458 |
4 |
856 |
10.2 |
486 |
5 |
801 |
21.9 |
441 |
6 |
859 |
11.4 |
479 |
7 |
848 |
13.6 |
468 |
8 |
833 |
6.8 |
456 |
9 |
892 |
8.2 |
497 |
10 |
940 |
5.9 |
520 |
11 |
783 |
5.8 |
462 |
12 |
736 |
9.7 |
386 |
[0055] These results give considerations as follows. Samples of Tests Nos. 1 to 7 are examples
which meet all conditions specified in the present invention and are found to offer
excellent high-temperature strength and to have better toughness. These samples are
also found to have sufficiently high steel surface hardness after the aging heat treatment.
[0056] In contrast, samples of Tests Nos. 8 to 12 are comparative examples which do not
meet one or more of the conditions specified in the present invention and offer at
least one of high-temperature strength, toughness, and surface hardness at poor level.
[0057] Specifically, the sample of Test No. 8 is a sample using Steel G, which has a ratio
([Mo]/[Ti]) of the Mo content to the Ti content of out of the range specified in the
present invention. This sample offers lower toughness even it has undergone an aging
heat treatment under appropriate conditions.
[0058] The sample of Test No. 9 is a sample using Steel H, which has a total content of
Mo and Ti of out of the range specified in the present invention. This sample offer
lower toughness even it has undergone an aging heat treatment under appropriate conditions.
[0059] The sample of Test No. 10 is a sample using Steel I, which has a total content of
Mo and Ti and a ratio ([Mo]/[Ti]) both out of the ranges specified in the present
invention. This sample offers lower toughness even it has undergone an aging heat
treatment under appropriate conditions.
[0060] The sample of Test No. 11 is a sample using Steel I, which has a total content of
Mo and Ti and a ratio ([Mo]/[Ti]) both out of the ranges specified in the present
invention. In addition, this sample has undergone an aging heat treatment for an excessively
long holding time. In this sample, the aging heat treatment condition causes the sample
to have lower toughness, although it does not so much affect the high-temperature
strength and the surface hardness.
[0061] The sample of Test No. 12 is a sample using Steel I, which has a total content of
Mo and Ti and a ratio ([Mo]/[Ti]) both out of the ranges specified in the present
invention. In addition, this sample has undergone an aging heat treatment at an excessively
high temperature for an excessively long holding time. This sample offers lower toughness,
is in the state of over-aging, and has a high-temperature strength and a surface hardness
not meeting the predetermined conditions (criteria).