[Technical Field]
[0001] The present disclosure relates to a wire rod for springs with high strength and excellent
corrosion fatigue resistance, a steel wire, and a method of manufacturing the same,
which may preferably be applied to a suspension spring, a torsion bar, and a stabilizer,
or the like, used for vehicles.
[Background Art]
[0002] Recently, it has been required to reduce weights of materials used for vehicles to
improve fuel efficiency of vehicles, and a suspension spring has been designed to
be manufactured using a high strength material having strength of 1800 MPa or higher
after a quenching and tempering process so as to respond to the demand for lightweight
materials.
[0003] Steel used for springs is formed as a spring through the following processes. After
manufacturing a wire rod through a hot rolling process, in case of a hot formed spring,
the wire rod is manufactured as a spring through a heating process, a forming process,
and a quenching and tempering process performed in order, and in case of a cold formed
spring, the wire rod is manufactured as a spring through a drawing process and a quenching
and tempering process performed in order.
[0004] Generally, when a material is designed to have high strength, toughness may be degraded
due to grain boundary embrittlement resistance, or for other reasons, and also, crack
sensitivity may increase. Thus, although high strength may be achieved, if corrosion
resistance of a material degrades, an externally exposed component, such as a suspension
spring of a vehicle, may have a corrosion pit created in a region in which paint is
removed, and the component may be damaged at an early stage due to fatigue cracks
spreading from the corrosion pit.
[0005] A corrosion environment of a suspension spring may be increased due to snow melting
agents used to prevent a road surface from freezing in winter. Accordingly, demand
for steel for springs with high strength and improved corrosion fatigue resistance
has increased.
[0006] Corrosion fatigue of a suspension spring refers to breakage of a spring. When paint
on the surface of a spring is removed due to pebbles on a road surface or foreign
objects, a material of the portion with no paint is exposed externally, which may
cause a pitting corrosion reaction, and a corrosion pit may be created and grown,
such that cracks may be generated and spread from the pit. Then, hydrogen from an
external source may be concentrated on the cracks and may cause hydrogen embrittlement,
which may lead to spring breakage.
[0007] To improve corrosion fatigue resistance of a spring, the method of increasing types
and amounts of contents of alloy elements have been used in the prior art. In reference
1, a content of Ni is increased to 0.55 weight% to improve corrosion resistance, thereby
increasing corrosion fatigue life, and in reference 2, a content of Si is increased
to create micronized carbide precipitated during tempering, thereby improving strength
against corrosion fatigue. In reference 3, Ti precipitation, a strong hydrogen trapping
site, and a V, Nb, Zr, and Hf precipitation, weak hydrogen trapping sites, are balanced
to improve hydrogen delayed fracture resistance, thereby improving a corrosion fatigue
life of a spring.
[0008] However, as Ni is an expensive element, material costs may increase when a large
amount of Ni is added. As for Si, Si is a representative element causing decarburization,
and thus, if a content of Si is increased, it may cause substantial risk. Ti, V, Nb,
and the like, elements creating precipitation, may degrade the corrosion fatigue life
because the elements may crystallize coarse carbonitrides from liquid materials when
the materials are solidified.
[0009] To achieve high strength of a spring, the method of adding alloy elements and the
method of decreasing a tempering temperature have been used in the prior art. As the
method of achieving high strength by adding alloy elements, the method of increasing
quenching hardness using C, Si, Mn, and Cr has been used, and strength of a steel
material may increase through a rapid cooling and a tempering heat treatment using
Mo, Ni, V, Ti, and Nb, and the like, relatively expensive alloy elements. The techniques,
however, may increase material costs.
[0010] Strength of a steel material has also been increased by changing heat treatment conditions
in a general component system without changing an alloy composition. When a tempering
temperature is deceased, strength of a material may increase. However, when a tempering
temperature decreases, an area reduction rate may decrease, which may cause degradations
in toughness, and may also cause early breakage of a spring while a spring is formed
and used, and other problems .
[0011] Thus, it has been necessary to develop a wire rod for springs with high strength
and excellent corrosion fatigue resistance, a steel wire, and a method of manufacturing
the same.
(Prior Art)
[0012]
(Reference 1) Japanese Laid-Open Patent Publication No. 2008-190042
(Reference 2) Japanese Laid-Open Patent Publication No. 2011-074431
(Reference 3) Japanese Laid-Open Patent Publication No. 2005-023404
[Disclosure]
[Technical Problem]
[0013] An aspect of the present disclosure is to provide a wire rod for springs with high
strength and excellent corrosion fatigue resistance, a steel wire, and a method of
manufacturing the same by controlling a combination of contents of Cr, Cu, and Ni
to a certain level, controlling a maximum depth of a corrosion pit to a certain level
or less, and controlling a content of fine carbide containing Mo to a certain level
or higher.
[0014] Meanwhile, the purposes of the present disclosure are not limited to the features
described above. The purposes of the present disclosure may be understood on the basis
of the descriptions in the specification, and it may not be difficult for a person
having skilled in the art in the field in which the present disclosure is included
to understand additional purposes of the present disclosure.
[Technical Solution]
[0015] An aspect of the present disclosure relates to a wire rod for springs with excellent
corrosion fatigue resistance including C: 0.40 to 0.70%, Si: 1.30 to 2.30%, Mn: 0.20
to 0.80%, Cr: 0.20 to 0.80%, Cu: 0.01 to 0.40%, Ni: 0.10 to 0.60%, Mo: 0.01 to 0.40%,
P: 0.02% or less, S: 0.015% or less, N: 0.01% or less, and a balance of Fe and inevitable
impurities by weight%, the wire rod satisfies equation 1 below,

where each element symbol is a value of a content of each element measured by weight%,
a microstructure comprises 50 area% or less of ferrite and a balance of pearlite,
and the wire rod comprises 8.0×10
4 count/mm
2 or higher of Mo-based carbides.
[0016] Another aspect of the present disclosure relates to a method of manufacturing a wire
rod for springs with excellent corrosion fatigue resistance including heating a billet
to 900 to 1100°C, the billet comprising C: 0.40 to 0.70%, Si: 1.30 to 2.30%, Mn: 0.20
to 0.80%, Cr: 0.20 to 0.80%, Cu: 0.01 to 0.40%, Ni: 0.10 to 0.60%, Mo: 0.01 to 0.40%,
P: 0.02% or less, S: 0.015% or less, N: 0.01% or less, and a balance of Fe and inevitable
impurities by weight% and satisfying equation 1 below, equation 1: -0.14 ≤ 0.70[Cr]
- 0.76[Cu] - 0.24[Ni] ≤ 0.47, where each element symbol is a value of a content of
each element measured by weight%, obtaining a wire rod by finishing-hot-rolling the
heated billet at 800 to 1000°C, and coiling the wire rod and cooling the wire rod
such that the time for maintaining the wire rod at a temperature in a range of 600
to 700°C is 31 seconds or longer.
[0017] Another aspect of the present disclosure relates to a steel wire for springs with
excellent corrosion fatigue resistance and a method of manufacturing the same.
[0018] The solutions described above do not necessarily list all of the features of the
present disclosure. Various features of the present disclosure, and advantages and
effects thereof will further be understood with reference to exemplary embodiments
described below.
[Advantageous Effects]
[0019] According to the present disclosure, a wire rod for springs with high strength and
excellent corrosion fatigue resistance, a steel wire, and a method of manufacturing
the same may be provided.
[Description of Drawings]
[0020]
FIG. 1 is a graph illustrating a relative corrosion fatigue life depending on a maximum
depth of a corrosion pit according to an example embodiment; and
FIG. 2 is a graph illustrating a relative corrosion fatigue life depending on the
number of Mo-based carbides according to an example embodiment.
[Best Mode for Invention]
[0021] Hereinafter, embodiments of the present disclosure will be described with reference
to the accompanied drawings. The present disclosure, however, may be modified to various
other embodiments, and the scope of the present disclosure may not be limited to exemplary
embodiments described below. These embodiments are provided to help those skilled
in the art to understand the present disclosure.
[0022] To address the issues described above, in the present disclosure, various effective
factors affecting corrosion resistance of steel for springs have been examined. Also,
corrosion fatigue is the breakage of a spring. When a corrosion pit is created as
paint on a surface of a spring is removed, cracks are generated and spread from the
corrosion pit, and hydrogen from outside is concentrated on the cracks such that a
spring may be broken. The present disclosure is suggested upon the grounds as below
in consideration of the issue described above.
[0023] Cr, one of alloy elements, is generally known as an element which may improve corrosion
resistance, but as a result of a salt water spraying test, corrosion fatigue resistance
was degraded when a content of Cr increased. Also, Cu and Ni made corrosion rust formed
on a surface of a material amorphous during a corrosion reaction such that a corrosion
speed decreased. Thus, to improve corrosion fatigue resistance of steel for springs,
it may be important to control combination of contents of Cr, Cu, and Ni to an appropriate
level.
[0024] Also, the greater the maximum depth of a corrosion pit generated on a surface of
a material in the corrosion reaction, the further the corrosion fatigue resistance
was degraded. Particularly, the narrower and deeper the width of a corrosion pit,
the further the corrosion fatigue resistance may degrade. Thus, to improve corrosion
fatigue resistance properties of steel for springs, it may be necessary to control
a maximum depth of a corrosion pit to a certain level or less.
[0025] In addition, to prevent hydrogen from outside from being concentrated on cracks,
it may be necessary to trap hydrogen using fine carbides, and carbides including alloy
elements of V, Ti, Nb, Mo, and the like, as main ingredients, not cementite, may be
used as the fine carbide. Also, nano-sized and fine Mo-based carbides precipitated
at 700°C or less may effectively trap hydrogen, and when carbides include V, Ti, Nb,
and other like, besides Mo, as main ingredients, the carbides may have an excellent
hydrogen trapping effect when Mo is contained.
[0026] Thus, in the present disclosure, a wire rod for springs with high strength and excellent
corrosion fatigue resistance, a steel wire, and a method of manufacturing the same
may be provided by controlling combination of contents of Cr, Cu, and Ni, controlling
a maximum depth of a corrosion pit to a certain level or less, and controlling a content
of fine carbide including Mo to a certain level or higher.
Wire Rod for Springs with Corrosion Fatigue Resistance
[0027] In the description below, a wire rod for springs with excellent corrosion fatigue
resistance will be described in greater detail.
[0028] A wire rod for springs with excellent corrosion fatigue may include C: 0.40 to 0.70%,
Si: 1.30 to 2.30%, Mn: 0.20 to 0.80%, Cr: 0.20 to 0.80%, Cu: 0.01 to 0.40%, Ni: 0.10
to 0.60%, Mo: 0.01 to 0.40%, P: 0.02% or less, S: 0.015% or less, N: 0.01% or less,
and a balance of Fe and inevitable impurities by weight%, the wire rod may satisfies
equation 1, a microstructure may include 50 area% or less of ferrite and a balance
of pearlite, and the wire rod may include 8.0×10
4 count/mm
2 or higher of Mo-based carbides.
[0029] In the description below, an alloy composition of the example embodiment will be
described in greater detail. In example embodiments, a unit of each element content
may be weight% unless otherwise indicated. Also, the alloy composition may be applied
to the method of manufacturing a wire rod, and may also be applied to a steel wire
and the method of manufacturing the steel wire.
C: 0.40 to 0.70%
[0030] C is an essential element added to secure strength of a spring. To draw the effect
of C, it may be preferable to add 0.40% or higher of C. When a content of C exceeds
0.70%, a twin-type martensite structure may be formed during a heat treatment in a
quenching and tempering process, and cracks may be created in a material, which may
significantly decrease fatigue life, may increase defect sensitivity, and may significantly
degrade fatigue life or fracture stress when a corrosion pit is created. Thus, a preferable
content of C may be 0.40 to 0.70%.
[0031] A more preferable lower limit content of C may be 0.45%, and a more preferable upper
limit content may be 0.65%.
Si: 1.30 to 2.30%
[0032] Si may be dissolved in ferrite, may enhance strength of a base material and may improve
deformation resistance.
[0033] When a content of Si is less than 1.30%, the effect of Si dissolved in ferrite to
enhance strength of a base material and to improve deformation resistance may be insufficient.
Thus, a preferable lower limit content of Si may be 1.30%, and a more preferable lower
limit may be 1.45%. When a content of Si exceeds 2.30%, the effect of improvement
in deformation resistance may be saturated such that no significant effect may be
obtained from additionally added Si, and surface decarburization may occur during
a heat treatment. Thus, a preferable upper limit content of Si may be 2.30%, and a
more preferable upper limit may be 2.25%.
Mn: 0.20 to 0.80%
[0034] If Mn is included in the steel material, Mn may secure strength of a steel material
by improving hardenability of the steel material.
[0035] When a content of Mn is less than 0.20%, it may be difficult to obtain sufficient
strength and hardenability required for a material for springs with high strength,
whereas, when a content of Mn exceeds 0.80%, hardenability may increase excessively
such that a martensite hard structure may easily be creased during cooling after a
hot rolling process, and MnS inclusions may increasingly be created, which may degrade
corrosion fatigue resistance properties. Thus, a preferable content of Mn may be 0.20
to 0.80%
[0036] A more preferable lower limit content of Mn may be 0.30%, and an even more preferable
lower limit content may be 0.40%. A more preferable upper limit content of Mn may
be 0.75%, and an even more preferable upper limit content may be 0.70%.
Cr: 0.20 to 0.80%
[0037] Cr may be used to prevent oxidation resistance, temper softening properties, and
surface decarburization and to secure hardenability.
[0038] When a content of Cr is less than 0.20%, it may be difficult to secure the sufficient
effect of oxidation resistance, temper softening properties, surface decarburization,
and hardenability. When a content of Cr exceeds 0.80%, deformation resistance may
degrade such that strength may degrade. Thus, a preferable content of Cr may be 0.20
to 0.80%.
[0039] A more preferable lower limit content of Cr may be 0.22%, and an even more preferable
upper limit may be 0.75%.
Cu: 0.01 to 0.40%
[0040] Cu may be added to improve corrosion resistance. When a content of Cu is less than
0.01%, the effect of improvement in corrosion resistance may be insufficient, whereas,
when a content of Cu exceed 0.40%, embrittlement may degrade during a hot rolling
process, which may cause cracks, and other problems . Thus, a preferable content of
Cu may be 0.01 to 0.40%. A more preferable content of Cu may be 0.05 to 0.30%.
Ni: 0.10 to 0.60%
[0041] Ni may be added to improve hardenability and toughness . When a content of Ni is
less than 0.10%, the effect of hardenability and toughness may not be sufficient,
whereas, when a content of Ni exceeds 0.60%, the amount of residual austenite may
increase, which may decrease fatigue life, and may increase manufacturing costs as
Ni is expensive. Thus, a preferable content of Ni may be 0.10 to 0.60%.
Mo: 0.01∼0.40%
[0042] Mo may contribute to refining microstructure by forming carbonitride together with
carbon or nitrogen, and may work as a trap site for hydrogen. To obtain the effect,
a preferable content of Mo may be 0.01% or higher. However, when a content of Mo is
excessive, it may be highly likely than a martensite hard structure may be created
during cooling after a hot rolling process, and coarse carbonitride may be created,
which may degrade flexibility of a steel material. Thus, a preferable upper limit
content of Mo may be 0.40%.
P: 0.02% or less
[0043] P is impurities. P may be segregated into a grain boundary and may degrade toughness.
Thus, it may be preferable to control an upper limit content of P to be 0.02%.
S: 0.015% or less
[0044] S is impurities. S may be segregated into a grain boundary as an element having a
low melting point and may degrade toughness, and may also create large amount of MnS,
which may degrade corrosion resistance properties of a spring. Thus, it may be preferable
to control an upper limit content of S to be 0.015%.
N: 0.01% or less
[0045] Nitride (N) may easily create BN by reacting with boron (B), and may decrease a quenching
effect, and thus, a content of N may need to be controlled to be relatively low. Considering
process load, it may be preferable to control a content of N to be 0.01% or less.
[0046] Iron (Fe) may also be added in the example embodiment. In a general manufacturing
process, unintended impurities from raw materials or a surrounding environment may
inevitably be added, and thus, Fe may not be excluded. A person skilled in the art
may be aware of such impurities, and thus, the impurities may not be described in
detail in the example embodiment.

(In equation 1, each element symbol is a value of a content of each element measured
by weight%)
[0047] Cr, Cu, and Ni may need to satisfy each element content described above, and may
also satisfy equation 1 above.
[0048] Cr is known as an element which may improve corrosion resistance, but as a content
of Cr increases in steel for springs, corrosion fatigue resistance may degrade. The
reason is that Cr may decrease pH of a pit bottom during a corrosion reaction such
that Cr may create a strongly acid atmosphere in the pit and may increase a maximum
depth of the pit. Thus, the higher the content of Cr, the more the corrosion fatigue
resistance may degrade.
[0049] Cu and Ni may make corrosion rust formed on a surface of a material amorphous in
a corrosion reaction such that Cu and Ni may decrease a corrosion speed. Thus, the
correlation between contents of Cr, Cu, and Ni and the decrease of corrosion fatigue
resistance of steel for springs was examined, and the effect rate of Cr was 0.70,
the effect rate of Cu was -0.76, and the effect rate of Ni was -0.24. By controlling
the correlation to satisfy equation 1 above, corrosion fatigue resistance was improved.
[0050] In addition to the alloy composition described above, one or more elements selected
from among V: 0.01 to 0.20%, Ti: 0.01 to 0.15%, and Nb: 0.01 to 0.10% may further
be added.
V: 0.01 to 0.20%
[0051] V may improve strength and may contribute to grain refinement. Further, V may work
as a trap site for hydrogen infiltrating steel by forming carbonitride together with
carbon (c) or nitrogen (N) and such that V may prevent hydrogen infiltration in steel
and may decrease corrosion of steel.
[0052] When a content of V is less than 0.01%, the above-described effect may not be sufficient.
When a content of V is excessive, manufacturing costs may increase. Thus, a preferable
upper limit content of V may be 0.20%.
Ti: 0.01 to 0.15%
[0053] Ti may improve spring properties by causing a precipitation hardening effect by forming
carbonitride, and may improve strength and toughness by refining grains and reinforcing
precipitation. Ti may also work as a trap site for hydrogen infiltrating steel such
that Ti may prevent hydrogen infiltration in steel and may decrease corrosion of steel.
[0054] When a content of Ti is less that 0.01 %, it may not be effective in that a frequency
of precipitations reinforcing precipitation and working as a hydrogen trap site decreases.
When a content of Ti exceeds 0.15%, manufacturing costs may significantly increase,
the effect of improvement in spring properties due to precipitations may be saturated,
and the amount of coarse alloy carbide which has not been dissolved into a base material
during a heat treatment of austenite such that the coarse alloy carbide may work as
a non-metal inclusion. Accordingly, the effect of fatigue properties and precipitation
reinforcement may degrade.
Nb: 0.01 to 0.10%
[0055] Nb may contribute to structure refinement by forming carbonitride together with carbon
or nitrogen, and may work as a trap site for hydrogen. To obtain the effect, a preferable
content of Nb may be 0.01% or higher. However, when a content of Nb is excessive,
coarse carbonitride may be formed, which may degrade ductility of steel. Thus, a preferable
upper limit content of Nb may be 0.10%.
[0056] A microstructure of a wire rod in the example embodiment may include 50 area% or
less of ferrite, and a balance of pearlite. The area fraction above was measured exclusive
of precipitation.
[0057] When an area fraction of ferrite exceeds 50 area%, strength of a material may significantly
decrease such that, after a final heat treatment, a desirable level of strength may
not be implemented.
[0058] Also, the remainder excluding ferrite is pearlite. When hard structure such as martensite
is existed in addition to ferrite and pearlite, a wire rod may be broken in a process
of drawing the wire rod.
[0059] The wire rod in the example embodiment may include 8.0×10
4 count/mm
2 or higher of Mo-based carbides.
[0060] To prevent hydrogen from outside from being concentrated on cracks, hydrogen may
need to be trapped using fine carbide, and carbide including alloy elements of V,
Ti, Nb, Mo, or the like, as main ingredients, not cementite, may be used as the fine
carbide. The carbide including Mo as a main ingredient may be precipitated in nano-size
within a temperature in a range of 600 to 700°C such that a hydrogen trapping effect
may significantly increase. When the carbides include V, Ti, Nb, and the like, as
main ingredients, a hydrogen trapping effect may significantly increase when Mo is
contained.
[0061] Thus, it may be preferable to include 8.0×10
4 count/mm
2 or higher of Mo-based carbides, and more preferably, 8.5×10
4 count/mm
2 or higher of Mo-based carbides may be included.
[0062] The number of Mo-based carbides may not be significantly changed when a steel wire
is manufactured, but the number of Mo-based carbides may decrease slightly. Thus,
it may be more preferable to secure 9.0×10
4 count/mm
2 or higher of Mo-based carbides in a wire rod state.
[0063] The Mo-based carbides may include 5 weight% or higher of Mo based on carbides. That
is because, as described above, when the carbides include V, Ti, Nb, and the like,
as main ingredients, a hydrogen trapping effect may significantly increase when Mo
is contained.
Method of Manufacturing Wire Rod for Springs with Excellent Corrosion Fatigue Resistance
[0064] In the description below, a method of manufacturing a wire rod for springs with excellent
corrosion fatigue resistance will be described in greater detail in accordance with
an example embodiment.
[0065] The method of manufacturing a wire rod for springs with excellent corrosion fatigue
resistance may include heating a billet satisfying the above-described alloy composition
to 900 to 1100°C, obtaining a wire rod by finishing-hot-rolling the heated billet
at 800 to 1000°C, and coiling the wire rod and cooling the wire rod such that the
time for maintaining the billet at a temperature in a range of 600 to 700°C may be
31 seconds or longer.
Heating Billet
[0066] The billet satisfying the above-described alloy composition may be heated to 900
to 1100°C.
[0067] The heating temperature of the billet may be 900°C or higher because, by melting
all coarse carbides generated during a molding process, the alloy elements may be
uniformly distributed in austenite. When a heating temperature of the billet exceeds
1100°C, the billet may be excessively heated such that heat consumption may increase,
and the time may be prolonged, which may cause excessive decarburization.
Hot-Rolling
[0068] A wire rod may be obtained by finishing-hot-rolling the heated billet to 800 to 1000°C.
[0069] The temperature of the finishing-rolling may be 800°C or higher to facilitate precipitation
of fine carbides. When the temperature of the finishing-rolling is less than 800°C,
load taken in a roller may increase, and when the temperature of the finishing-rolling
exceeds 1000°C, a size of a grain may increase such that toughness may degrade, and
transformation may be delayed in a cooling process, and accordingly, martensite hard
structure may be created.
Coiling and Cooling
[0070] After the wire rod is coiled, the wire rod may be cooled such that the time for maintaining
the wire rod at a temperature in a range of 600 to 700°C may be 31 seconds or longer.
[0071] The reason for controlling the time for maintaining the wire rod at a temperature
in a range of 600 to 700°C to be 31 seconds or longer may be to secure sufficient
time for completing pearlite transformation without creating martensite hard structure
during a cooling process, and to sufficiently precipitate fine carbides including
Mo as a main ingredient.
Steel Wire for Springs with Excellent Corrosion Fatigue Resistance
[0072] A steel wire for springs with excellent corrosion fatigue resistance in an example
embodiment may satisfy the above-described alloy composition, a microstructure may
be a tempered martensite single phase, and the steel wire may include 8.0×10
4 count/mm
2 or higher of Mo-based carbides. As a microstructure is a tempered martensite single
phase, and 8.0×10
4 count/mm
2 or higher of Mo-based carbides are included, corrosion fatigue resistance may improve.
The tempered martensite single phase may refer to a structure mostly formed of tempered
martensite with a balance of an inevitable impure structure.
[0073] To prevent hydrogen from outside from being concentrated on cracks, hydrogen may
need to be trapped using fine carbides, and carbides including alloy elements of V,
Ti, Nb, Mo, or the like, as main ingredients, not cementite, may be used as the fine
carbides. The carbides including Mo as a main ingredient may be precipitated in nano-size
within a temperature in a range of 600 to 700°C such that a hydrogen trapping effect
may significantly increase, and when carbides include V, Ti, Nb, or the like, as main
ingredients, a hydrogen trapping effect may significantly increase when Mo is contained.
Thus, it may be preferable to include 8. 0×10
4 count/mm
2 or higher of Mo-based carbides, and more preferably, 8.5×10
4 count/mm
2 or higher of Mo-based carbides may be included. The Mo-based carbides may be created
when a wire rod is manufactured, and the Mo-based carbides may not be changed but
may slightly decrease during a heating process and a cooling process when a steel
wire is manufactured.
[0074] A maximum depth of a corrosion pit of the steel wire in the example embodiment may
be 120 µm or less.
[0075] In a corrosion reaction, the deeper the maximum depth of a corrosion pit created
on a surface of a material, the more the corrosion fatigue resistance properties of
steel for springs may degrade. Particularly, the narrower and deeper the corrosion
pit, the greater the stress applied to the pit, which may significantly degrade corrosion
fatigue resistance.
[0076] The maximum depth of the corrosion pit may be measured after 14 repetitions of a
cycle in which a sample of the steel wire was put in a salt water spray tester, 5%
salt water was sprayed onto the steel wire sample for 4 hours in an atmosphere at
35°C, the steel wire sample was dried for 4 hours at atmosphere at a temperature of
25°C and humidity of 50%, and the steel wire sample was wet for 16 hours until humidity
became 100%. The harshest condition was set in consideration of usage environment
of steel for springs, and when a maximum depth of the corrosion pit is 120 µm or less
under the above-described conditions, improved corrosion fatigue resistance could
be secured.
[0077] The tensile strength of steel wire in the example embodiment may be 1800MPa or higher.
Method of Manufacturing Steel Wire for Springs with Excellent Corrosion Fatigue Resistance
[0078] A method of manufacturing a steel wire for springs with excellent corrosion fatigue
resistance in an example embodiment may include obtaining a steel wire by drawing
the wire rod manufactured by the method of manufacturing a wire rod described in the
aforementioned example embodiment, austenitizing the steel wire by heating the steel
wire to 850∼1000°C and maintaining the heated steel wire for 1 minute or longer, and
oil-cooling the austenitized wire rod to 25 to 80°C and tempering the wire rod at
350 to 500°C.
[0079] When the maintaining time after heating is less than 1 minute, structures of ferrite
and pearlite may not be sufficiently heated such that the wire rod may not be transferred
to be austenite, and thus, it may be preferable to control the heating time to be
1 minute or longer. Also, the oil-cooling temperature is generally used condition,
and thus, the oil-cooling temperature may not be particularly limited.
[0080] When the tempering temperature is less than 350°C, toughness may not be secured,
and accordingly, the wire rod may be broken during a forming process and in a product
state. When the tempering temperature exceeds 500°C, strength may degrade. Thus, a
preferable tempering temperature may be 350 to 500°C.
[Mode for Invention]
[0081] In the description below, embodiments of the present disclosure will be described
in greater detail. It should be noted that the exemplary embodiments are provided
to describe the present disclosure in greater detail, and to not limit the scope of
rights of the present disclosure. The scope of rights of the present disclosure may
be determined on the basis of the subject matters recited in the claims and the matters
reasonably inferred from the subject matters.
[0082] A billet having a composition as in Table 1 below was heated to 1000°C, and was coiled
after finishing-rolling at 900°C. In a cooling process after coiling, a temperature
in a range of 600 to 700°C was maintained for maintaining times listed in Table 2
below, and a wire rod was manufactured. A microstructure of the wire rod was observed
and listed in Table 2 below.
[0083] The wire rod was drawn, was heated at 975°C for 15 minutes, was put in oil of 70°C
and was rapidly cooled, and the cooled wire rod was maintained at 390°C for 30 minutes,
and a steel wire was manufactured.
[0084] Tensile strength of the steel wire, a maximum depth of a corrosion pit, a Mo-based
carbide, and relative corrosion fatigue life were measured and listed in Table 2 below.
All microstructures were martensite single phases.
[0085] The tensile strength was measured by, after gathering tensile samples of the steel
wire in accordance with ASTM E 8 standard, performing a tensile test.
[0086] As for the Mo-based carbide, the sample was cut cross-sectionally, fine carbides
were extracted by a replica method, and the fine carbides were analyzed using a transmission
electron microscope and energy dispersive X-ray spectroscopy, and the number of carbides
including 5% or higher of Mo from the result was listed in Table 1 below.
[0087] A cycle in which a sample of the steel wire was put in a salt water spray tester,
5% salt water was sprayed onto the steel wire sample for 4 hours at atmosphere of
35°C, the steel wire sample was dried for 4 hours at atmosphere of temperature of
25°C and humidity of 50%, and the steel wire sample was wet for 16 hours until humidity
became 100% was repeated 14 times, and a maximum depth of a corrosion pit and a relative
corrosion fatigue life were measured.
[0088] A maximum depth of a corrosion pit was measured using a confocal laser microscope.
[0089] The relative corrosion fatigue life was measured by performing a rotary bending fatigue
test, a speed of the fatigue test was 3, 000 rpm, and a weight applied to the sample
was 40% of tensile strength. 10 samples were tested for corrosion fatigue life, and
fatigue lives of 8 samples excluding the sample having the highest fatigue life and
the sample having the lowest fatigue life were averaged. The average value was determined
as a corrosion fatigue life of the respective sample. Relative corrosion fatigue lives
of the other samples of when a corrosion fatigue life of a comparative example 1 was
1 were listed in Table 2.
[Table 1]
| Steel Type |
Alloy Composition (Weight%) |
Equation 1 |
| C |
Si |
Mn |
Cr |
Cu |
Ni |
Mo |
P |
S |
N |
V |
Ti |
Nb |
| Comparative Steel 1 |
0.53 |
1.53 |
0.68 |
0.73 |
- |
- |
- |
0.016 |
0.008 |
0.0049 |
|
|
|
0.51 |
| Comparative Steel 2 |
0.50 |
1.49 |
0.51 |
0.11 |
0.22 |
0.25 |
- |
0.009 |
0.005 |
0.0052 |
0.11 |
|
|
-0.15 |
| Comparative Steel 3 |
0.63 |
1.62 |
0.40 |
0.26 |
0.28 |
0.62 |
0.16 |
0.010 |
0.010 |
0.0042 |
|
0.02 |
|
-0.18 |
| Comparative Steel 4 |
0.55 |
1.85 |
0.61 |
0.86 |
0.10 |
0.19 |
0.14 |
0.011 |
0.007 |
0.0051 |
0.10 |
|
0.03 |
0.48 |
| Comparative Steel 5 |
0.48 |
2.26 |
0.59 |
0.28 |
0.34 |
0.58 |
0.22 |
0.008 |
0.007 |
0.0046 |
0.08 |
0.03 |
|
-0.20 |
| Inventive Steel 1 |
0.52 |
1.51 |
0.68 |
0.72 |
0.14 |
0.21 |
0.03 |
0.012 |
0.008 |
0.0045 |
|
|
|
0.35 |
| Inventive Steel 2 |
0.49 |
1.45 |
0.48 |
0.23 |
0.22 |
0.52 |
0.13 |
0.008 |
0.006 |
0.0057 |
|
|
|
-0.13 |
| Inventive Steel 3 |
0.60 |
1.52 |
0.43 |
0.28 |
0.15 |
0.56 |
0.16 |
0.010 |
0.004 |
0.0044 |
0.18 |
|
0.02 |
-0.05 |
| Inventive Steel 4 |
0.53 |
1.68 |
0.41 |
0.33 |
0.21 |
0.25 |
0.36 |
0.013 |
0.006 |
0.0054 |
|
0.14 |
|
0.01 |
| Inventive Steel 5 |
0.49 |
2.17 |
0.64 |
0.71 |
0.06 |
0.10 |
0.25 |
0.009 |
0.007 |
0.0047 |
0.12 |
|
0.05 |
0.43 |
[0090] In Table 1 above, equation 1 indicates values of 0.70[Cr] - 0.76[Cu] - 0.24[Ni].

[0091] In Table 2 above, F refers to ferrite, P refers to pearlite, and M refers to martensite.
[0092] Inventive Examples 1 to 5 which satisfied the alloy composition and manufacturing
conditions described in the present disclosure had excellent tensile strength and
relative corrosion fatigue life. Relative corrosion fatigue lives of the comparative
examples were between 0.97 and 1.28, but relative corrosion fatigue lives of the Inventive
Examples were between 3.23 and 8.21, which were significantly increased.
[0093] The comparative examples secured 1800MPa or higher of tensile strength, but did not
satisfy the alloy composition and manufacturing conditions described in the present
disclosure, and accordingly, relative corrosion fatigue lives were deteriorated.
[0094] Maximum depths of corrosion pits of the comparative examples were 128 µm or greater,
and the numbers of Mo-based carbides turned out to be less than 8 x 10
4 count/mm
2.
[0095] As in comparative examples 6 and 7, if the alloy composition described in the example
embodiment was not satisfied, even when the manufacturing conditions described in
the example embodiment were satisfied, relative corrosion fatigue lives were relatively
low. Also, as in comparative examples 8 and 9, even when the alloy composition described
in the example embodiment was satisfied, but when the maintaining time at 600 to 700°C
was not satisfied, relative corrosion fatigue lives were relatively low.
[0096] Also, when a martensite hard structure was formed in a wire rod state as in comparative
examples 3 to 5, 8, and 9, breakage of the wire rod frequently occurred during a drawing
process, and accordingly, it was difficult to manufacture the wire rod as a steel
wire.
[0097] FIG. 1 is a graph illustrating a relative corrosion fatigue life depending on a maximum
depth of a corrosion pit according to an example embodiment. The smaller the maximum
depth of a corrosion pit, the greater the relative corrosion fatigue life, and when
a maximum depth of a corrosion pit is greater than 120 µm, relative corrosion fatigue
life was significantly degraded.
[0098] FIG. 2 is a graph illustrating a relative corrosion fatigue life depending on the
number of the Mo-based carbides. The higher the number of Mo-based carbides, the greater
the relative corrosion fatigue life was increased, and when the number of the Mo-based
carbides was smaller than 8.0×10
4 count/mm
2, relative corrosion fatigue life significantly was degraded.
[0099] While exemplary embodiments have been shown and described above, the scope of the
present disclosure is not limited thereto, and it will be apparent to those skilled
in the art that modifications and variations could be made without departing from
the scope of the present invention as defined by the appended claims.