[0001] The present invention relates to a stainless steel sheet product, which is useful
as a member or part driven under environmental conditions with a fear of delayed fracture
derived from penetration of hydrogen due to its excellent properties such as corrosion-resistance,
surface hardness, toughness and fatigue strength, and also relates to a manufacturing
method thereof.
[0002] 18%Ni maraging steel, which is a representative steel material with hardness of HV450
or more, has a single phase of martensite in a quenched state. It is hardened by aging.
Good wear-resistance and fatigue strength are applied to the steel by nitriding to
harden a surface layer.
[0003] Although 18%Ni maraging steel is very hard, it is poor of toughness and ductility
due to a single phase of martensite. Due to poor toughness and ductility, fatigue
strength is insufficient, and delayed fracture originated in interstitial hydrogen
often occurs in presence of inclusions. In order to overcome these disadvantages,
severe selection of raw materials and also special processes involving high-vacuum
melting and secondary refining are necessary for reduction of impurities to a possible
lowest level. As a result, 18%
Ni maraging steel has been prepared with lower productivity at a higher cost, as compared
with conventional steel.
[0004] The element
Ti is often added as an aging promoter to 18%
Ni maraging steel, but increases inclusions of titanium compound unfavorable for fatigue
strength of 18%
Ni maraging steel.
[0005] The present invention aims at provision of a high-strength and tough stainless steel
product having surface hardness of HV450 or more and being improved in delayed fracture
strength by combination of a specified alloying design and manufacturing conditions.
[0006] The present invention proposes a new stainless steel product suitable for this purpose.
The proposed stainless steel product contains 12.0-18.0 mass %
Cr and 4.0-10.0 mass %
Ni. Its metallurgical structure comprises a matrix of strain-induced martensite, in which
residual austenite grains are dispersed at a rate of 20 vol. % or more. The residual
austenite grains as well as prior austenite grains are elongated with an aspect ratio
of 3 at least. The stainless steel product has a surface layer hardened to HV450 or
more in the state that a half-value width of (200) α' X-ray diffraction peak is 0.30
degrees at least.
[0007] The stainless steel sheet product is manufactured by solution-annealing the semi-stable
austenitic stainless steel sheet, cold-rolling the annealed stainless steel sheet
at a reduction ratio of 35-65%, and then optionally aging or nitride-aging the rolled
steel sheet at 300-650°C. Nitride-aging is performed by a gas-nitriding process or
a salt bath process. According to the gas-nitriding process, a stainless steel sheet
is heated at 300-650°C in a nitrogen atmosphere. According to the salt bath process,
a stainless steel sheet is immersed in a salt bath, which contains one or more of
NaCN, KCN, NaCNO and
KCNO as basic components, and held at 300-650°C.
[0008] When a solution-annealed stainless steel sheet is welded to a ring shape and then
cold-rolled by a ring rolling mill, a steel belt good of fatigue strength suitable
for a continuously variable transmission is manufactured.
[0009] The inventors have continued various researches and experiments for development of
a stainless steel sheet endurable under severe conditions with a fear of interstitial
hydrogen, and discovered that a semi-stable austenitic stainless steel sheet having
a dual phase structure of strain-induced martensite and austenite is suitable for
the purpose instead of conventional martensite steel sheet having a single phase of
martensite. The stainless steel sheet is further improved in resistance to hydrogen
embrittlement and delayed fracture by conditioning it to the metallurgical structure,
wherein residual austenite grains are dispersed in a matrix of strain-induced martensite
at a rate of 20 vol. % at least, and modifying its surface layer to a hardened state
of HV450 or more. The residual austenite grains as well as prior austenite grains
are preferably elongated with an aspect ratio of 3 at least by cold-rolling. A surface
layer of the stainless steel sheet product is preferably modified to the state that
a half-value width of (200) α' X-ray diffraction peak is 0.30 degrees or broader.
[0010] Increase of residual austenite grains in a matrix of strain-induced martensite promotes
dissolution of hydrogen in the austenite grains, and diffusion speed of hydrogen is
lower in an austenite phase than a martensite phase. Dissolution of hydrogen means
decrease of active hydrogen effecting on fracture and also retards motion of hydrogen
atoms in the steel matrix. An effect of the austenite phase on delayed fracture derived
from interstitial hydrogen is apparently recognized by lowering a rate of the strain-induced
martensite below 80 vol. %.
[0011] Diffusion of an element generally occurs at grain boundaries with ease rather than
inside grains, and hydrogen is also diffused along grain boundaries. Diffusion of
hydrogen from one grain to an adjacent grain along grain boundaries is drastically
retarded in the case where an aspect ratio of the grains is 3 or more. The effect
of the aspect ratio on diffusion of hydrogen will be explained as follows:
[0012] Dislocation density is basically high at grain boundaries, and strains are predominantly
accumulated at the grain boundaries as increase of the aspect ratio. The high dislocation
density and accumulation of strains extremely delays diffusion of hydrogen and enhances
resistance to delayed fracture originated in interstitial hydrogen.
[0013] Transgranular dislocations are also effective for trapping hydrogen atoms diffused
into a steel matrix. Trapping of hydrogen atoms is intensified as increase of transgranular
dislocations, so as to suppress delayed fracture. A degree of dislocations accumulated
in grains can be quantitatively represented as a half-value width of (200) diffraction
peak by analyzing a steel sheet product with α' X-ray.
[0014] The other features of the present invention as well as alloying elements and manufacturing
conditions will be understood from the following explanation:
Alloying Design
C up to 0.20 mass %
[0015] C is an austenite former, which suppresses generation of δ-ferrite in a high-temperature
region and also strengthens a martensite phase induced by cold-rolling. Solubility
limit of
C is lowered as increase of
Si content in the inventive alloy system. Excessive inclusion of
C promotes precipitation of coarse chromium carbide particles, which put harmful influences
on intergranular corrosion resistance and fatigue strength, during aging. In this
sense,
C content is preferably controlled to 0.20 mass % at most.
1.0-5.0 mass % of Si
[0016] Si is an alloying element useful as a deoxidizing agent at a steelmaking stage, and
Si content derived from the deoxidizing agent has been controlled to 1.0 mass % at most
as noted in such work-hardened stainless steel as
SUS301 or
SUS304. Increase of
Si content on the contrary is favorable in the inventive stainless steel, so as to promote
generation of strain-induced martensite during cold-rolling. The element
Si also hardens the strain-induced martensite. Moreover, residual austenite grains are
hardened by dissolution of
Si. Consequently, the stainless steel sheet is substantially strengthened by cold-rolling.
The element
Si is also effective in combination with
Cu for promotion of age-hardening. These effects are typically noted by addition of
Si at a ratio of 1.0 mass % or more. However, excessive addition of
Si above 5.0 mass % causes high-temperature cracking and brings out various troubles
in a manufacturing process. In this sense,
Si content is preferably controlled within a range of 1.0-5.0 mass %.
Mn up to 5.0 mass %
[0017] Mn is an alloying element, which raises stability of an austenite phase.
Mn content is determined to a ratio in balance with the other alloying elements. However,
excessive addition of
Mn above 5.0 mass % unfavorably suppresses generation of strain-induced martensite during
cold-rolling.
4.0-10.0 mass % of Ni
[0018] Although
Ni is an alloying element necessary for maintenance of an austenite phase at high and
low temperatures in general, the inventive stainless steel is based on the alloying
design that an austenite phase semi-stable at a room temperature is partially transformed
to strain-induced martensite by cold-rolling.
Ni content is determined within a range of 4.0-10.0 mass % from such the alloying design.
Shortage of
Ni means excessive generation of δ-ferrite in a high-temperature region and transformation
to martensite in a cooling step. As a result, an austenite phase cannot be maintained
in a stainless steel sheet cooled down to a room temperature. Surplus of
Ni on the contrary stabilizes an austenite phase to an extent unfavorable for generation
of strain-induced martensite.
12.0-18.0 mass % of Cr
[0019] Cr is an alloying element effective for corrosion resistance, and
Cr content of 12.0 mass % at least is necessary for corrosion resistance suitable for
the purpose. However, excessive addition of
Cr above 18.0 mass % causes excessive generation of δ-ferrite in a high-temperature
region, since
Cr is a ferrite former. Although generation of δ-ferrite can be suppressed by addition
of austenite formers such as
C, N, Ni, Mn and
Cu, addition of austenite formers means stabilization of an austenite phase at a room
temperature and suppresses generation of strain-induced martensite during cold-rolling.
Excessive addition of austenite formers also puts harmful influences on increase of
strength during aging. In this sense,
Cr content is determined within a range of 12.0-18.0 mass %.
Cu up to 3.5 mass %
[0020] Cu is an optional element effective for promotion of age-hardening in combination with
Si. But, excessive addition of
Cu above 3.5 mass % worsens hot-workability of a stainless steel sheet and also causes
occurrence of cracks.
Mo up to 5.0 mass %
[0021] Mo is an optional element for improvement of corrosion resistance and also promotes
dispersion of fine carbonitride particles during aging. Abrupt release of strains
is favorably suppressed by Mo during high-temperature aging treatment, which is a
processing step suitable for releasing surplus of strains induced by cold-rolling
but harmful on fatigue strength. Since the fine carbonitride particles precipitated
by aging favorably increase strength of a stainless steel sheet, the stainless steel
sheet can be aged at a relatively higher temperature without decrease of strength.
However, excessive addition of Mo causes generation of δ-ferrite in a high-temperature
region, and deformation resistance (in other words, hot-workability) at a high-temperature
region becomes bigger as increase of
Mo content. In this sense,
Mo content is preferably determined at a ratio up to 5.0 mass %.
N up to 0.15 mass %
[0022] N is an austenite former effective for hardening austenite and martensite phases, but
excessive inclusion of
N causes occurrence of blow holes in a casting step. In this sense,
N content is preferably determined at a ratio up to 0.15 mass %.
Metallurgical Structure of Cold-Rolled Stainless Steel Sheet Rates of strain-induced
martensite and residual austenite
[0023] An amount of hydrogen dissolved in a steel matrix becomes bigger as decrease of strain-induced
martensite (in other words, increase of residual austenite), since diffusion of hydrogen
is slower in austenite grains than martensite grains. As a result, an absolute amount
of active hydrogen harmful on fracture strength is reduced, and motion of the active
hydrogen is also restricted, so as to suppress delayed fracture. Such an effect of
decrease of strain-induced martensite on delayed fracture property is apparently noted,
when a rate of strain-induced martensite is reduced to 80 vol. % or less in a cold-rolled
stainless steel sheet.
Aspect ratio of austenite grains
[0024] In general, density of dislocations is high at grain boundaries, and predominant
accumulation of strains is more intensified as a bigger aspect ratio of grains. Such
grain boundaries and the bigger aspect ratio are effective for retarding diffusion
of hydrogen and inhibiting delayed fracture originated in interstitial hydrogen. These
effects on delayed fracture are typically noted at an aspect ratio of 3 at least in
the inventive alloy system. Density of dislocations in grains.
[0025] Transgranular dislocations trap hydrogen atoms and favorably suppress delayed fracture.
Density of transgranular dislocations can be evaluated as a half-value width of (200)
α' X-ray diffraction peak, since the width becomes broader as increase of dislocations
accumulated in grains at a surface layer of a stainless steel sheet product. The effect
of transgranular dislocations on delayed fracture is clearly noted, when the width
is of 0.30 degrees at least.
Manufacturing Conditions
Cold-rolling
[0026] A stainless steel sheet, which is cold-rolled with a too-small reduction ratio, is
poor of surface hardness with insufficient accumulation of dislocations evaluated
as a half-value width of (200) α' X-ray diffraction peak. A reduction ratio of 35
% at least is necessary for raising the half-value width to an effective level for
delayed fracture strength. A surface layer of the stainless steel sheet is also hardened
to HV450 or more by the cold-rolling, resulting in improvement of fatigue strength.
In this sense, a reduction ratio is preferably determined within a range of 35-65%
in the cold-rolling step. A too-high reduction ratio above 65 % leads to excessive
generation of strain-induced martensite and worsens various properties of a stainless
steel sheet product.
[0027] After a semi-stable austenite stainless steel sheet is cold-rolled under the conditions
to generate strain-induced martensite at a controlled ratio and to accumulate strains
in crystal grains with a proper aspect ratio, it is aged or nitride-aged for improvement
of surface hardness and fatigue strength. Aging or nitride-aging is preferably performed
at 300-650°C in 20 minutes. If the stainless steel sheet is heated at a temperature
lower than 300°C, an effect of aging or nitride-aging on strength is insufficient.
But, a higher temperature above 650°C leads to partial inversion of strain-induced
martensite to austenite, resulting in lowering of strength and retard of nitriding
reaction.
[0028] Nitride-aging may be performed by a conventional process, which has been applied
to steel material. For instance, gas nitriding, gas soft-nitriding, gas nitrosulphurizing,
plasma nitriding, salt-bath nitriding, ion-nitriding, salt-bath carbonitriding, salt-bath
nitrosulphurizing, etc.
[0029] In the gas nitriding process, sole ammonia gas or mixed gas based on ammonia is used
as a nitriding gas. The mixed gas based on ammonia may be prepared by mixing ammonia
gas with
RX gas (endothermic modified gas:
CO+H2+N2), NX gas (modified gas produced by complete combustion of butane and based on nitrogen),
propane, butane or mixture of (
CO2+CO). The salt-bath nitriding process uses a molten salt prepared by adding one or both
of
Na2CO3 and
K2CO3 to one or more of basic components selected from
NaCN, KCN, NaCNO and
KCNO.
EXAMPLE
[0030] Several semi-stable austenite stainless steels having compositions shown in
Table 1 were melted in a vacuum furnace. Each stainless steel was cast to a slab, forged,
hot-rolled, annealed and then cold-rolled. Steels
A, B and
C belong to semi-stable austenite stainless steel defined by the present invention,
while steel
D corresponds to 18%
Ni maraging steel for comparison.
[0031] After each cold-rolled steel sheet was solution-annealed 1 minute at 1050°C and quenched
in water, it was cold-rolled to thickness of 0.18 mm with various reduction ratios
by a ring-rolling mill. Thereafter, the steel sheets were processed by barreling,
shot-peening, shot-blasting or combination thereof. Some steel sheets were finally
aged or nitride-aged. Nitride-aging was performed in a nitrogen atmosphere of 50 vol.
%
NH3 and 50 vol. %
NX gas or in a salt bath consisting of 40 mass %
NaCN, 40 mass %
Na2CO3 and the balance being
(NaK)4Fe(CN)O6.
Table 1:
Chemical Composition Of Austenite Stainless Steels |
Steel Kind |
Alloying Elements (mass %) |
|
C |
Si |
Mn |
Ni |
Cr |
Cu |
Mo |
Ti |
Co |
N |
A |
0.077 |
2.23 |
0.45 |
7.54 |
16.22 |
0.24 |
1.25 |
0.01 |
0.01 |
0.074 |
B |
0.082 |
2.68 |
0.28 |
8.25 |
13.56 |
0.16 |
2.25 |
0.01 |
0.00 |
0.080 |
C |
0.040 |
1.35 |
1.43 |
5.34 |
14.25 |
1.89 |
0.98 |
0.01 |
0.01 |
0.087 |
D |
0.005 |
0.02 |
0.03 |
18.24 |
0.05 |
0.02 |
5.02 |
0.44 |
9.08 |
0.002 |
[0032] A test piece of 20 mm in length and 20 mm in width sampled from each steel sheet
was electrolytically polished and then subjected to X-ray analysis to detect a half-value
width of (200) α' X-ray diffraction peak. The X-ray analysis was performed with a
scanning speed of 0.2 degrees/minute under accelerating voltage of 40kV and an electric
current of 120A.
[0033] Surface hardness of each test piece in a finish-annealed state was measured by Vickers
hardness meter with a load of 300g.
[0034] A rate of residual austenite grains in each test piece was measured by a magnetic
method using an oscillating magnetometer.
[0035] An aspect ratio of prior austenite grains was calculated as follows: 100 grains were
sampled at random from elongated austenite grains, which were observed on a cross
section of a test piece cut off along a rolling direction. A major axis
D1 and a minor axis
D2 of each elongated austenite grain along the rolling direction and a vertical direction,
respectively, were measured. Quotient
D1/D2 was calculated per every sampled austenite grains. A mean value of the quotients
D1/D2 was regarded as an aspect ratio of prior austenite grains.
[0036] Ring-shaped test pieces of 350 mm in length and 15 mm in width were sampled from
each steel sheet. A lubricant was applied to test pieces, and two test pieces were
overlapped together and examined by such a rotary fatigue test as follows:
[0037] The overlapped test pieces were hung on a driven pulley of 40.0 mm in diameter and
fixed to a belt, which was stretched between the driven pulley and a drive pulley,
at both ends. The driven pulley was rotated at 800 rpm in the state that the test
pieces were stretched by the belt. Fatigue strength of the test piece was evaluated
as a cycle number until fracture of the test pieces. Test pieces, which were not fractured
even after 1000×10
4 cycles, were regarded as material good of fracture strength.
[0038] Test results of cold-rolled steel sheets are shown in
Table 2, while those of aged or nitride-aged steel sheets are shown in
Table 3.

[0039] Results in
Tables 2 and
3 prove that the inventive stainless steel sheets are good of fatigue strength, i.e.
≥400 × 10
4 cycles by the rotary fracture test.
[0040] On the other hand,
Sample Nos. 8-10 were poor of fatigue strength, since density of strains accumulated at grain boundaries
were insufficient due to small reduction ratios in addition to small aspect ratios.
Sample Nos. 11 and
13 were also poor of fatigue strength, since strain-induced martensite grains were excessively
generated due to a high reduction ratio of 70%.
[0041] When
Sample Nos. 8-10 (cold-rolled steel sheets) were observed by a microscope, cracks originated in poor
strength were detected in grains at fracture planes.
Sample No. 11 (a cold-rolled steel sheet) and
Sample Nos. 20-25 (aged or nitride-aged steel sheets) were cracked at grain boundaries. Change from
transgranular to intergranular cracking is probably explained by increase of strength
due to aging or nitride-aging. Such intergranular cracking is a kind of typical delayed
fracture caused by penetration of hydrogen into steel ring material from a lubricant
between two overlapped steel rings.
[0042] It is understood from these results that delayed fracture was suppressed by properly
controlling an aspect ratio of prior austenite grains, surface hardness in a finish-annealed
state and a rate of residual austenite as well as introduction of rolling strains.
Although
Inventive Sample Nos. 15 and
18 were broken, fracture is transgranular with a ductile fracture plane.
[0043] According to the present invention as mentioned above, a semi-stable austenite stainless
steel sheet is cold-rolled with a predetermined reduction ratio so as to promote transformation
to strain-induced martensite. An aspect rate of prior austenite grains, a rate of
residual austenite, surface hardness in a finish-annealed state and modification of
a surface layer to a state appropriate for inhibiting diffusion of hydrogen are realized
by the controlled cold-rolling, so that the cold-rolled steel sheet product is improved
in strength and toughness as well as delayed fracture strength. The stainless steel
sheet product manufactured in this way is useful as a member or part for various kinds
of springs for automobiles, e.g. a metal gasket or a ring for a belt of a continuously
variable transmission, a steel belt, a blade, a separator for a fuel cell, a leaf
spring and so on.
1. A stainless steel sheet product excellent in strength, toughness and delayed fracture
strength, which:
consists of 12.0-18.0 mass % Cr, 4.0-10.0 mass % Ni, 0.20 mass % or less C, 1.0∼5.0 mass % Si, 5.0 mass % or less Mn, optionally one or more selected from Cu of up to 3.5 mass%, Mo of up to 5.0 mass%, N of up to 0.15 mass % and the balance
being Fe except inevitable impurities;
comprises the metallurgical structure that residual austenite grains are present in
a strain-induced martensite matrix at a rate of 20 vol. % or more, said austenite
grains and also prior austenite grains being elongated with an aspect ratio of 3 or
more; and
has a surface layer hardened above HV450 and modified to the state that a half-value
width of (200) α' X-ray diffraction peak is 0.30 degrees at least.
2. A method of manufacturing a stainless steel sheet product excellent in strength, toughness
and delayed fracture strength, which comprises the steps of:
providing a semi-stable austenitic stainless steel containing 12.0-18.0 mass % Cr, 4.0-10.0 mass % Ni, 0.20 mass % or less C, 1.0∼5.0 mass % Si, 5.0 mass % or less Mn, optionally one or more selected from Cu of up to 3.5 mass %, Mo of up to 5.0 mass%, N of up to 0.15 mass% and the balance being Fe except inevitable impurities;
solution-annealing said stainless steel;
cold-rolling the solution-annealed stainless steel with a reduction ratio of 35-65%
so as to promote transformation to strain-induced martensite; and
optionally processing said cold-rolled stainless steel by barreling, shot peening,
shot blasting or combination thereof,
whereby the stainless steel is reformed to the metallurgical structure that residual
austenite grains are present in a strain-induced martensite matrix at a rate of 20
vol. % or more, said austenite grains and also prior austenite grains being elongated
with an aspect ratio of 3 or more, and a surface layer being hardened above HV450
and modified to the state that a half-value width of (200) α' X-ray diffraction peak
is 0.30 degrees at least.
3. The manufacturing method as defined in Claim 2, wherein the stainless steel sheet
is cold-rolled by a ring rolling mill.
4. The manufacturing method as defined in Claim 2 or 3, wherein the stainless steel sheet
is further aged or nitride-aged at 300-650°C after cold-rolling.
5. The manufacturing method as defined in Claim 4, wherein the stainless steel sheet
is nitride-aged in a nitrogen atmosphere.
6. The manufacturing method as defined in claim 4, wherein the stainless steel sheet
is nitride-aged in a salt bath based on one or more of NaCN, KCN, NaCNO and KCNO.