TECHNICAL FIELD
[0001] The present invention relates to steel, and more particularly relates to a steel
for machine structural use.
BACKGROUND ART
[0002] Excellent rolling contact fatigue properties may be required for machine components
to be used for structural use and power transmission use, such as components of general
machinery and automobiles. An example of a method for producing such kind of machine
components is as follows. A steel for machine structural use is subjected to hot working
(hot forging or the like) to produce an intermediate product. The intermediate product
is subjected to machining (cutting or grinding) to produce a machine component. There
are also cases in which, as necessary, the machine component is subjected to a heat
treatment (normalizing or the like), a case hardening heat treatment (induction hardening
or the like), or quenching and tempering. A steel for machine structural use for producing
such kind of machine components is required to be excellent in machinability.
[0003] A steel for machine structural use that is excellent in machinability is also called
a "free-cutting steel", and is defined in JIS G 4804 (2008) (Non Patent Literature
1). The machinability of a free-cutting steel is enhanced by containing Pb.
[0004] A steel for machine structural use that contains Pb is disclosed, for example, in
Japanese Patent Application Publication No.
2000-282172 (Patent Literature 1). The steel material for machine structural use disclosed in
Patent Literature 1 has a chemical composition which contains, in mass%, C: 0.05 to
0.55%, Si: 0.50 to 2.5%, Mn: 0.01 to 2.00%, S: 0.005 to 0.080%, Cr: 0 to 2.0%, P:
0.035% or less, V: 0 to 0.50%, N: 0.0150% or less, Al: 0.04% or less, Ni: 0 to 2.0%,
Mo: 0 to 1.5%, B: 0 to 0.01%, Bi: 0 to 0.10%, Ca: 0 to 0.05%, Pb: 0 to 0.12%, Ti:
0 to less than 0.04%, Zr: 0 to less than 0.04% and Ti (%) + Zr (%): 0 to less than
0.04%, Te: 0 to 0.05%, Nd: 0 to 0.05%, Nb: 0 to 0.1%, Cu: 0 to 1.5%, and Se: 0 to
0.5%, the chemical composition satisfying a condition that a value of fn1 represented
by a formula hereunder is 100 or less, a value of fn2 represented by a formula hereunder
is 0 or more, and a value of fn3 represented by a formula hereunder is 3.0 or more,
with the balance being Fe and impurities. In addition, a proportion that a ferritic
phase occupies in the micro-structure is, with respect to the area ratio, from 10
to 80%, and Hv hardness is in a range from 160 to 350. Here, fn1 = 100C+11Si+18Mn+32Cr+45Mo+6V,
fn2 =-23C+Si(5-2Si)-4Mn+104S-3Cr-9V+10, and fn3 = 3.2C+0.8Mn+5.2S+0.5Cr-120N+2.6Pb+4.1Bi-0.001α
2+0.13α. A symbol of an element in the respective formulas represents the content in
mass% of the corresponding element, and α represents the area ratio (%) of the ferritic
phase in the micro-structure. It is described in Patent Literature 1 that the steel
material for machine structural use is excellent in machinability and toughness.
CITATION LIST
PATENT LITERATURE
[0005] Patent Literature 1: Japanese Patent Application Publication No.
2000-282172
NON PATENT LITERATURE
[0006] Non Patent Literature 1: Japanese Industrial Standards Committee, Standard No.: JIS
G 4804 (2008), Standard Name: Free-cutting Steels
SUMMARY OF INVENTION
TECHNICAL PROBLEM
[0007] In this connection, in some cases machining such as cutting is performed using an
automated equipment system. In an automated equipment system, in the case of producing
a large amount of machine components by cutting intermediate products, such as producing
several hundred or more machine components per day, excellent chip treatability is
required. It is preferable that chips that are to be discharged accompanying cutting
are split into small pieces and discharged. If the chips remain connected in a long
length, the chips are liable to become entwined around the intermediate product, and
defects are liable to arise on the surface of the machine component after cutting.
If a chip is entwined around a machine component, it is also necessary to temporarily
stop the production line to remove the chip that is entwined around the machine component.
In this case, it is difficult to perform unattended production, and it is necessary
to assign personnel to monitor the production process. Thus, chip treatability affects
both the quality of the machine components and the production cost. In addition, in
an automated equipment system, productivity decreases as tool wear increases. Therefore,
a steel for machine structural use is required to have high machinability, such as
being capable of suppressing tool wear and being excellent in chip treatability.
[0008] In addition, when cutting is performed using automated equipment system, in some
cases rust occurs in the machine component. In an automated equipment system, a water-soluble
cutting oil is utilized from the viewpoint of performing unattended operations. Consequently,
in some cases rust occurs in the machine components. Rust is not only a cause of the
occurrence of shape errors, but is also a cause of quality defects when performing
a plating treatment on the machine component. In addition, after cutting, the machine
components are sometimes stored in a bucket or the like for a long time period until
undergoing the next process after the cutting process. For example, in a case where
machine components are cut in a certain country and the next process is performed
in a separate factory in a different country, a period of several days to several
months may pass after cutting until the machine components are subjected to the next
process. Therefore, a steel for machine structural use is required to be not only
excellent in machinability, but also to have characteristics that suppress the occurrence
of rust (hereunder, referred to as "rusting characteristics").
[0009] An objective of the present invention is to provide a steel for machine structural
use that is excellent in machinability and rusting characteristics, and with which
a machine component that is excellent in rolling contact fatigue properties is obtained.
SOLUTION TO PROBLEM
[0010] A steel for machine structural use according to the present invention has a chemical
composition which consists of, in mass%, C: 0.30 to 0.50%, Si: 0.01 to 0.80%, Mn:
0.20 to 2.00%, P: 0.030% or less, S: 0.010 to 0.100%, Pb: 0.010 to 0.100%, Al: 0.010
to 0.050%, N: 0.015% or less, O: 0.0005 to 0.0030%, Cr: more than 0.70% to 2.00%,
Ni: 0 to 3.50%, B: 0 to 0.0050%, V: 0 to 0.70%, Mo: 0 to 0.70%, W: 0 to 0.70%, Nb:
0 to less than 0.050%, Cu: 0 to 0.50%, Ti: 0 to 0.100% and Ca: 0 to 0.0030%, with
the balance being Fe and impurities, the chemical composition satisfying Formula (1).
In the steel, a total number of specific inclusions which are any of MnS inclusions,
Pb inclusions, and composite inclusions containing MnS and Pb and which have an equivalent
circular diameter of 5 µm or more is 40 per mm
2 or more.

[0011] Where, a content (mass%) of a corresponding element is substituted for each symbol
of an element in Formula (1).
ADVANTAGEOUS EFFECTS OF INVENTION
[0012] A steel for machine structural use according to the present invention is excellent
in machinability and rusting characteristics, and is a steel with which a machine
component that is excellent in rolling contact fatigue properties is obtained.
BRIEF DESCRIPTION OF DRAWINGS
[0013]
FIG. 1A is a schematic diagram illustrating an S distribution in an observation surface,
that was obtained by EPMA analysis.
FIG. 1B is a schematic diagram illustrating a Pb distribution in the same observation
surface as in FIG. 1A, that was obtained by EPMA analysis.
FIG. 1C is a schematic diagram of an image obtained by combining FIG. 1A and FIG.
1B.
FIG. 2 is a schematic diagram for describing a criterion for determining whether or
not to regard adjacent inclusions as a single inclusion.
FIG. 3 is a transverse sectional view of a starting material that was cast.
FIG. 4 is a schematic diagram of a cutting test machine for describing a cutting test.
FIG. 5A is a perspective view of a chip.
FIG. 5B is a planar photographic view of a chip.
FIG. 6 shows a front view and a side view of a rolling contact fatigue test specimen
used in a rolling contact fatigue test.
FIG. 7 is a schematic diagram of a thrust-type rolling contact fatigue test machine
for describing a rolling contact fatigue test.
DESCRIPTION OF EMBODIMENTS
[0014] The present inventors conducted investigations and studies regarding the machinability
and rusting characteristics of steels for machine structural use. As a result, the
present inventors found that if a steel for machine structural use has a chemical
composition consisting of, in mass%, C: 0.30 to 0.50%, Si: 0.01 to 0.80%, Mn: 0.20
to 2.00%, P: 0.030% or less, S: 0.010 to 0.100%, Pb: 0.010 to 0.100%, Al: 0.010 to
0.050%, N: 0.015% or less, O: 0.0005 to 0.0030%, Cr: more than 0.70% to 2.00%, Ni:
0 to 3.50%, B: 0 to 0.0050%, V: 0 to 0.70%, Mo: 0 to 0.70%, W: 0 to 0.70%, Nb: 0 to
less than 0.050%, Cu: 0 to 0.50%, Ti: 0 to 0.100%, and Ca: 0 to 0.0030%, with the
balance being Fe and impurities, excellent machinability is obtained, and that there
is a possibility that excellent rolling contact fatigue properties will be obtained
after quenching and tempering.
[0015] Mn in the steel combines with S to form MnS. The MnS is divided into MnS inclusions
and MnS precipitates according to the formation process. MnS inclusions crystallize
in the molten steel before solidification. On the other hand, MnS precipitates precipitate
in the steel after solidification. The MnS inclusions form in the molten steel. Therefore,
the size of the MnS inclusions tends to be large in comparison to the MnS precipitates
that form after solidification.
[0016] On the other hand, most of the Pb in the steel does not dissolve in the steel, and
is present as Pb inclusions (Pb grains). The MnS inclusions and Pb inclusions each
enhance the machinability of the steel.
[0017] In addition, in a case where Mn and Pb are present in the steel, in addition to the
aforementioned MnS inclusions and Pb inclusions, the Mn and Pb also form composite
inclusions containing MnS and Pb (hereinafter, also referred to simply as "composite
inclusions"). The term "composite inclusions" means inclusions that contain MnS and
Pb, with the balance being impurities. More specifically, there are cases where composite
inclusions are composed by MnS and Pb that are adjacent to each other, and there are
also cases where Pb dissolves into MnS to form a composite inclusion. In the present
description, "MnS inclusions", "Pb inclusions" and "composite inclusions" are identified
by a method described in a section "Method of measuring number of inclusions TN and
RA" which is described later. In the present description, the term "MnS inclusions"
refers to inclusions that contain Mn and S and do not contain Pb. The term "Pb inclusions"
refers to inclusions which are composed of Pb and impurities and which do not contain
Mn. The term "composite inclusions" refers to inclusions that contain Mn, S and Pb.
[0018] MnS inclusions are known as inclusions that enhance machinability. On the other hand,
the fusing point of Pb inclusions is lower than the fusing point of MnS inclusions.
Therefore, Pb inclusions exert a lubricating action during cutting, and as a result
the machinability of the steel is enhanced.
[0019] In addition, it is considered that composite inclusions enhance the machinability
of steel more than individual MnS inclusions and Pb inclusions. In a case where a
fissure has arisen at the periphery of a composite inclusion, liquefied Pb enters
into the open crack. By this means, propagation of the crack is promoted and machinability
is enhanced. Accordingly, if composite inclusions are also formed, and not just MnS
inclusions and Pb inclusions, the machinability is enhanced further.
[0020] The mechanism by which composite inclusions are formed is considered to be as follows.
It is easier for Pb to move in liquid phase than in solid phase. Therefore, almost
no composite inclusions can be formed from MnS precipitates which form after solidification
of the steel, and the composite inclusions are instead formed by adherence of Pb to
MnS inclusions that are formed in the molten steel before solidification. Accordingly,
in order to form a large number of composite inclusions, it is desirable to form a
large number of MnS inclusions in the molten steel rather than forming MnS precipitates
after solidification.
[0021] As described above, in order to enhance the machinability of steel, it suffices to
form a large number of MnS inclusions, Pb inclusions and composite inclusions. As
described above, MnS inclusions are formed in molten steel by crystallization. In
addition, as described above, the greater the number of MnS inclusions that are present,
the greater the number of composite inclusions that will be formed. Therefore, it
is considered that the machinability of the steel is enhanced by causing a large number
of MnS inclusions to crystallize in the molten steel.
[0022] On the other hand, a steel for machine structural use that contains MnS inclusions,
MnS precipitates, Pb inclusions and composite inclusions is susceptible to rusting.
However, hitherto the mechanism of rusting with respect to a steel for machine structural
use had not been studied in detail. Therefore the present inventors conducted investigations
and studies regarding the rusting mechanism. As a result, the present inventors obtained
the following finding.
[0023] MnS inclusions, MnS precipitates, Pb inclusions and composite inclusions become
starting points for rust. In this case, the susceptibility to rusting depends more
on the total number of MnS inclusions, MnS precipitates, Pb inclusions and composite
inclusions than the size of the MnS inclusions, MnS precipitates, Pb inclusions and
composite inclusions. Specifically, the susceptibility to rusting of the steel increases
as the total number of MnS inclusions, MnS precipitates, Pb inclusions and composite
inclusions increases. Based on the above finding, the present inventors concluded
that in order to suppress rusting while obtaining excellent machinability, it is effective
to decrease the total number of MnS inclusions, MnS precipitates, Pb inclusions and
composite inclusions. Therefore, the present inventors studied methods for decreasing
the total number of MnS inclusions, MnS precipitates, Pb inclusions and composite
inclusions.
[0024] As described above, MnS inclusions that are formed by crystallization in molten steel
are liable to grow (coarsen) in the molten steel. Therefore, the size of MnS inclusions
is larger than the size of MnS precipitates that are formed by precipitation in the
steel after solidification. That is, the MnS precipitates precipitate more finely
than the MnS inclusions. Therefore, in a steel having a certain Mn content and S content,
if a case in which MnS inclusions are caused to crystallize and a case in which MnS
precipitates are caused to precipitate are supposed, the number of MnS precipitates
that are formed by precipitation will be noticeably greater than the number of MnS
inclusions that are formed by crystallization. Accordingly, to improve the rusting
characteristics of a steel, it suffices to suppress precipitation of MnS precipitates
by crystallizing MnS inclusions in the molten steel and causing the MnS inclusions
to grow (coarsen).
[0025] In order to cause MnS inclusions to crystallize and grow in molten steel and suppress
precipitation of MnS precipitates and, as a result, decrease the total number of MnS
inclusions, MnS precipitates, Pb inclusions and composite inclusions, it suffices
to significantly increase the Mn content in comparison to the S content. If the Mn
content is sufficiently higher than the S content, coarse MnS inclusions are likely
to form in the molten steel. In this case, because S is consumed by the crystallization
of the coarse MnS inclusions, the amount of dissolved S in the steel after solidification
is lowered. Consequently, precipitation of MnS precipitates can be suppressed, and
the total number of MnS inclusions, MnS precipitates, Pb inclusions and composite
inclusions can be decreased. As a result, excellent rusting characteristics are obtained.
[0026] Specifically, the Mn content and S content satisfy the following Formula (1).

[0027] Where, the content (mass%) of a corresponding element is substituted for each symbol
of an element in Formula (1).
[0028] Here, it is defined that F1 = Mn/S. If F1 is less than 8.0, it is difficult for MnS
inclusions to adequately crystallize in the molten steel. Therefore the amount of
dissolved S in the steel after solidification cannot be adequately decreased, and
a large number of fine MnS precipitates are formed after solidification. In this case,
because the total number of MnS inclusions, MnS precipitates, Pb inclusions and composite
inclusions cannot be decreased, the rusting characteristics of the steel decline.
On the other hand, if F1 is 8.0 or more, the Mn content is adequately high in comparison
with the S content. In this case, by using an appropriate production method, MnS inclusions
in the molten steel adequately crystallize and grow. As a result, the amount of dissolved
S in the steel after solidification is adequately decreased, and precipitation of
MnS precipitates in the steel after solidification can be suppressed. Therefore, the
total number of MnS inclusions, MnS precipitates, Pb inclusions and composite inclusions
can be adequately reduced, and the rusting characteristics of the steel are enhanced.
[0029] Here, inclusions which are any of MnS inclusions, Pb inclusions and composite inclusions
and which have an equivalent circular diameter of 5 µm or more are defined as "specific
inclusions". In the present description, the term "equivalent circular diameter" means
the diameter of a circle in a case where the area of an inclusion or a precipitate
that is observed during micro-structure observation is converted into a circle having
the same area. In this case, in the present embodiment, in addition, in a steel for
machine structural use having the aforementioned chemical composition and satisfying
Formula (1), the total number of specific inclusions is 40 per mm
2 or more.
[0030] If the total number of specific inclusions in the steel is 40 per mm
2 or more, coarse MnS inclusions adequately crystallize and formation of MnS precipitates
can be suppressed. As a result, the total number of MnS inclusions, MnS precipitates,
Pb inclusions and composite inclusions which become starting points for rusting can
be adequately reduced. Therefore, excellent machinability and excellent rusting characteristics
can both be realized in a compatible manner. On the other hand, if the total number
of specific inclusions in the steel is less than 40 per mm
2, MnS inclusions do not adequately crystallize, and a large number of MnS precipitates
form. As a result, the formation of MnS precipitates can be suppressed. Consequently,
the total number of MnS inclusions, MnS precipitates, Pb inclusions and composite
inclusions which become starting points for rusting cannot be adequately reduced.
Therefore, although excellent machinability is obtained, adequate rusting characteristics
are not obtained.
[0031] A steel for machine structural use according to the present embodiment that was completed
based on the above findings has a chemical composition which consists of, in mass%,
C: 0.30 to 0.50%, Si: 0.01 to 0.80%, Mn: 0.20 to 2.00%, P: 0.030% or less, S: 0.010
to 0.100%, Pb: 0.010 to 0.100%, Al: 0.010 to 0.050%, N: 0.015% or less, O: 0.0005
to 0.0030%, Cr: more than 0.70% to 2.00%, Ni: 0 to 3.50%, B: 0 to 0.0050%, V: 0 to
0.70%, Mo: 0 to 0.70%, W: 0 to 0.70%, Nb: 0 to less than 0.050%, Cu: 0 to 0.50%, Ti:
0 to 0.100% and Ca: 0 to 0.0030%, with the balance being Fe and impurities, the chemical
composition satisfying Formula (1). In the steel, the total number of specific inclusions
which are any of MnS inclusions, Pb inclusions, and composite inclusions containing
MnS and Pb, and which have an equivalent circular diameter of 5 µm or more is 40 per
mm
2 or more.

[0032] Where, the content (mass%) of a corresponding element is substituted for the respective
elements in Formula (1).
[0033] The chemical composition of the steel for machine structural use that is described
above may contain one or more types of element selected from a group consisting of
Ni: 0.02 to 3.50%, B: 0.0005 to 0.0050%, V: 0.05 to 0.70%, Mo: 0.05 to 0.70%, W: 0.05
to 0.70%, Nb: 0.001 to less than 0.050%, Cu: 0.05 to 0.50% and Ti: 0.003 to 0.100%.
[0034] The chemical composition of the steel for machine structural use that is described
above may contain Ca: 0.0001 to 0.0030%.
[0035] In the steel for machine structural use that is described above, a ratio of the number
of the composite inclusions to the specific inclusions may be 40% or more.
[0036] Hereunder, the steel for machine structural use according to the present embodiment
is described in detail. The symbol"%" in the chemical composition means "mass percent"
unless specifically stated otherwise.
[Chemical Composition]
[0037] The chemical composition of the steel for machine structural use of the present embodiment
contains the following elements.
C: 0.30 to 0.50%
[0038] Carbon (C) increases the strength of steel. When producing a component using a steel
for machine structural use, as necessary, a heat treatment (normalizing or the like),
a case hardening heat treatment (induction hardening or the like), or quenching and
tempering are performed after forging the steel for machine structural use. In such
a case, C increases the strength of the steel. If the C content is less than 0.30%,
sufficient strength will not be obtained. If a soft steel is used, in some cases chips
connect during cutting, and the chips become entwined around the tools or material
and cause damage thereto. In addition, if the C content is less than 0.30%, the cutting
resistance also increases. On the other hand, if the C content is more than 0.50%,
the strength before quenching and tempering will be high, and the machinability of
the steel will decrease. Furthermore, if the C content is more than 0.50%, in a case
where a large amount of an alloying element other than C is contained, a supercooled
structure such as martensite will be formed. In such a case, the quality will become
nonuniform, and defects are liable to arise during cold working. Accordingly, the
C content is in the range of 0.30 to 0.50%. A preferable lower limit of the C content
is 0.35%, and more preferably is 0.40%. A preferable upper limit of the C content
is 0.45%, and more preferably is 0.42%.
Si: 0.01 to 0.80%
[0039] Silicon (Si) deoxidizes the steel. By adding Si after adding Mn at the time of deoxidation,
the Si modifies oxides. Specifically, Si added to molten steel modifies oxides that
are mainly composed of Mn into oxides that are mainly composed of Si. By adding Al
after adding Si, composite oxides containing Si and Al form in the steel. The composite
oxides serve as nuclei for crystallization of MnS inclusions. Therefore, the composite
oxides enhance the rusting characteristics of the steel. Si also enhances temper softening
resistance and raises the strength. The aforementioned effects are not obtained if
the Si content is less than 0.01%.
[0040] On the other hand, Si is a ferrite forming element. If the Si content is more than
0.80%, the outer layer of the steel may be decarburized. Furthermore, if the Si content
is more than 0.80%, the ferrite fraction may increase and the strength decrease in
some cases. Accordingly, the Si content is from 0.01 to 0.80%. A preferable lower
limit of the Si content for increasing the temper softening resistance is 0.10%, and
more preferably is 0.20%. A preferable upper limit of the Si content for keeping the
ferrite fraction low is 0.70%, and more preferably is 0.50%.
Mn: 0.20 to 2.00%
[0041] Manganese (Mn) forms MnS inclusions and composite inclusions containing MnS and Pb,
and enhances the machinability of the steel.
[0042] Mn also deoxidizes the steel. The deoxidizing power of Mn is weak compared to Si
or Al. Therefore, a large amount of Mn may be contained. In a case where another strong
deoxidizing element is not present in the molten steel, oxides that are mainly composed
of Mn form in the molten steel. Thereafter, if another strong deoxidizing element
(Si or Al) is added to the molten steel, the Mn contained in the oxides is discharged
into the molten steel, and the oxides are modified. Hereunder, the modified oxides
are referred to as "composite oxides". The Mn that is discharged into the molten steel
from the oxides combines with S to form MnS inclusions. Note that, composite oxides
formed by modification of oxides easily become nuclei for crystallization of MnS inclusions.
Therefore, if composite oxides are formed, crystallization of MnS inclusions is promoted.
The MnS inclusions formed by crystallization easily form composite inclusions also.
[0043] If the Mn content is less than 0.20%, it is difficult for MnS inclusions to adequately
crystallize. Therefore, a large number of MnS precipitates will form in the steel
after solidification. In this case, the total number of MnS inclusions, MnS precipitates,
Pb inclusions and composite inclusions will increase. Consequently, the rusting characteristics
of the steel will decrease. In contrast, if the Mn content is more than 2.00%, the
hardenability of the steel will be too high and, as a result, the hardness of the
steel will be too high. In this case, the machinability of the steel will decrease.
Accordingly, the Mn content is from 0.20 to 2.00%. A preferable lower limit of the
Mn content is 0.50%. A preferable upper limit of the Mn content is 1.50%, and more
preferably is 1.20%.
P: 0.030% or less
[0044] Phosphorus (P) is unavoidably contained. P embrittles the steel and enhances the
machinability. On the other hand, if the P content is more than 0.030%, hot ductility
decreases. In such a case, rolling defects and the like occur, and the productivity
decreases. Accordingly, the P content is 0.030% or less. A preferable lower limit
of the P content for enhancing the machinability is 0.005%. In this case, the machinability,
particularly the chip treatability, is enhanced. A preferable upper limit of the P
content is 0.015%.
S: 0.010 to 0.100%
[0045] Sulfur (S) forms MnS in the steel and enhances the machinability. In particular,
MnS suppresses tool wear. If the S content is less than 0.010%, MnS will not crystallize
adequately and it will be difficult for composite inclusions containing MnS and Pb
to form. As a result, the rusting characteristics will decrease. On the other hand,
if the S content is more than 0.100%, S will segregate at grain boundaries and the
steel will become brittle, and the hot workability of the steel will decrease. Accordingly,
the S content is from 0.010 to 0.100%. When prioritizing mechanical properties over
machinability, a preferable lower limit of the S content is 0.015%, and a preferable
upper limit is 0.030%. When prioritizing machinability, a preferable lower limit of
the S content is 0.030%, and a preferable upper limit is 0.050%.
Pb: 0.010 to 0.100%
[0046] Lead (Pb) forms Pb inclusions (Pb grains) by itself, and enhances the machinability
of the steel. Pb also combines with MnS inclusions to form composite inclusions and
enhance the machinability of the steel, and in particular enhance the chip treatability.
The aforementioned effects are not obtained if the Pb content is less than 0.010%.
On the other hand, if the Pb content is more than 0.100%, because the Pb inclusions
increase excessively, the rusting characteristics of the steel decrease. In addition,
if the Pb content is more than 0.100%, although the machinability is enhanced, the
steel becomes brittle. As a result, the hot workability of the steel will decrease.
Accordingly, the Pb content is from 0.010 to 0.100%. A preferable lower limit of the
Pb content for promoting the formation of composite inclusions and enhancing the machinability
is 0.020%, and more preferably is 0.025%. A preferable upper limit of the Pb content
for enhancing the rusting characteristics is 0.050%.
Al: 0.010 to 0.050%
[0047] Aluminum (Al) deoxidizes the steel. In the steel for machine structural use according
to the present invention, in order to suppress the formation of holes and surface
defects during solidification, deoxidation is performed by aluminum killing. As described
later, if deoxidation is performed by adding Al into the molten steel after Mn and
Si, oxides in the steel are modified and composite oxides containing Si and Al are
formed. The composite oxides easily become nuclei for crystallization of MnS inclusions.
Therefore, it is easy for MnS inclusions to disperse and crystallize, and to grow
and coarsen, and it is also easy for composite inclusions containing MnS and Pb to
form. In this case, the machinability of the steel improves. In addition, in a case
where MnS inclusions disperse and crystallize, precipitation of fine MnS precipitates
is suppressed. In this case, the total number of MnS inclusions, MnS precipitates,
Pb inclusions and composite inclusions increases. Consequently, the rusting characteristics
of the steel improve. Al also combines with N to form AlN and thereby suppress coarsening
of austenite grains in various kinds of heat treatment. The aforementioned effects
are not obtained if the Al content is less than 0.010%.
[0048] On the other hand, if the Al content is more than 0.050%, coarse composite oxides
are liable to form. If coarse composite oxides are formed in the steel, surface defects
are liable to occur on the steel. If coarse composite oxides are formed in the steel,
the fatigue strength of the steel will also decrease. In addition, if the Al content
is more than 0.050%, deoxidation will proceed excessively, and the amount of oxygen
in the molten steel will decrease. In this case, it will be difficult to form MnS
inclusions, and the machinability (particularly, suppression of tool wear) of the
steel will decrease. In such a case, in addition, it will be difficult for composite
inclusions in which Pb is combined with MnS inclusions to form, and a large number
of independent Pb inclusions will remain in the steel. As a result, the total number
of MnS inclusions, MnS precipitates, Pb inclusions and composite inclusions will increase,
and the rusting characteristics will decrease. Accordingly, the Al content is from
0.010 to 0.050%. A preferable lower limit of the Al content for obtaining a further
effect of suppressing the coarsening of grains by formation of AlN is 0.015%, and
more preferably is 0.020%. A preferable upper limit of the Al content is 0.035%. In
the present description, the term "Al content" means the content of acid-soluble Al
(sol. Al).
N: 0.015% or less
[0049] Nitrogen (N) is unavoidably contained. N combines with Al to form AlN to thereby
suppress coarsening of austenite grains during heat treatment and enhance the strength
of the steel. On the other hand, if the N content is more than 0.015%, the cutting
resistance of the steel increases and the machinability decreases. If the N content
is more than 0.015%, the hot workability also decreases. Accordingly, the N content
is 0.015% or less. A preferable lower limit of the N content is 0.002%, and more preferably
is 0.004%. A preferable upper limit of the N content is 0.012%, and more preferably
is 0.008%. In the present description, the term "N content" means the total content
of N (t-N).
O: 0.0005 to 0.0030%
[0050] Oxygen (O) is contained not only in oxides, but also in MnS inclusions. O forms composite
oxides that serve as nuclei for crystallization of MnS inclusions. If the O content
is less than 0.0005%, the formed amount of composite oxides will be insufficient,
and it will be difficult for MnS inclusions to crystallize in the molten steel. In
such a case, the machinability of the steel will decrease. Furthermore, in such a
case, a large number of fine MnS precipitates will form after solidification. As a
result, the total number of MnS inclusions, MnS precipitates, Pb inclusions and composite
inclusions will increase, and rusting characteristics will decrease. On the other
hand, if the O content is more than 0.0030%, in some cases coarse oxides that become
the starting points for fractures are formed. In this case, the rolling contact fatigue
properties of the steel decrease. Furthermore, if the O content is more than 0.0030%,
coarse alumina-based oxides will form and promote cutting wear of the tools, and hence
the machinability of the steel will decrease. Accordingly, the O content is from 0.0005
to 0.0030%. A preferable lower limit of the O content for further improving the machinability
of the steel as well as the rusting characteristics of the steel is 0.0007%, and more
preferably is 0.0010%. A preferable upper limit of the O content is 0.0025%, and more
preferably is 0.0020%. In the present description, the term "O content" means the
total content of oxygen (t-O).
Cr: more than 0.70% to 2.00%
[0051] Chromium (Cr) dissolves in the steel and enhances the hardenability and temper softening
resistance of the steel to thereby increase the strength of the steel. As a result,
the rolling contact fatigue properties of the steel are enhanced. In a case where
quenching and tempering are performed after hot forging, Cr deepens the hardened layer
depth. The aforementioned effects are not obtained if the Cr content is 0.70% or less.
On the other hand, if the Cr content is more than 2.00%, the hardenability will be
too high and a supercooled structure (martensite) will form during cooling and the
steel will become too hard. In such a case, the machinability of the steel will decrease.
If the Cr content is more than 2.00%, in some cases austenite may stabilize at even
a low temperature and the steel will become brittle. If the Cr content is more than
2.00%, in a case where induction hardening is performed, cementite will not dissolve
and the hardenability will decrease. Accordingly, the Cr content is more than 0.70%
to 2.00%. A preferable lower limit of the Cr content is 0.90%, and more preferably
is 1.00%. A preferable upper limit of the Cr content is 1.80%, and more preferably
is 1.60%.
[0052] The balance of the chemical composition of the steel for machine structural use according
to the present embodiment is Fe and impurities. Here, the term "impurities" refers
to elements which, during industrial production of the steel for machine structural
use, are mixed in from ore or scrap that is used as a raw material, or from the production
environment or the like, and which are allowed within a range that does not adversely
affect the steel for machine structural use of the present embodiment.
[Optional Elements]
[0053] The chemical composition of the steel for machine structural use of the present embodiment
may further contain one or more types of element selected from the group consisting
of Ni, B, V, Mo, W, Nb, Cu and Ti.
Ni: 0 to 3.50%
[0054] Nickel (Ni) is an optional element and need not be contained. If contained, Ni dissolves
in the steel and increases the hardenability of the steel, and enhances the steel
strength. Ni also improves the ductility of the matrix. In addition, Ni increases
the toughness of the steel. Furthermore, Ni increases the corrosion resistance of
the steel. The aforementioned effects are obtained to a certain extent if even a small
amount of Ni is contained. On the other hand, if the Ni content is more than 3.50%,
a large amount of retained austenite will remain. In such a case, a part of the retained
austenite will transform into martensite by strain induced transformation, and the
ductility of the steel will decrease. Accordingly, the Ni content is from 0 to 3.50%.
[0055] A preferable lower limit of the Ni content for stably obtaining the aforementioned
effects is 0.02%, and more preferably is 0.05%. A preferable upper limit of the Ni
content for further suppressing the formation of retained austenite is 2.50%, and
more preferably is 2.00%. When prioritizing toughness, a preferable lower limit of
the Ni content is 0.20%. Note that, Ni detoxifies Cu and enhances the toughness. If
the steel contains Cu, a preferable lower limit of the Ni content is equal to or more
than the Cu content.
B: 0 to 0.0050%
[0056] Boron (B) is an optional element and need not be contained. If contained, B increases
the hardenability of the steel and increases the steel strength. B also suppresses
segregation at the grain boundaries of P and S that decrease toughness, and thus enhances
the fracture characteristics. The aforementioned effects are obtained to a certain
extent if even a small amount of B is contained. On the other hand, if the B content
is more than 0.0050%, a large amount of BN will be formed and the steel will become
brittle. Accordingly, the B content is from 0 to 0.0050%. A preferable lower limit
of the B content in a case where Ti or Nb that are nitride-forming elements is contained
is 0.0005%. A preferable upper limit of the B content is 0.0020%.
V: 0 to 0.70%
[0057] Vanadium (V) is an optional element and need not be contained. If contained, V precipitates
as V carbides, V nitrides, or V carbo-nitrides during tempering and during nitriding,
and enhances the strength of the steel. The V precipitates (V carbides, V nitrides
and V carbo-nitrides) also suppress coarsening of austenite grains and increase the
toughness of the steel. In addition, V dissolves in the steel and thereby increases
the temper softening resistance of the steel. The aforementioned effects are obtained
to a certain extent if even a small amount of V is contained.
[0058] On the other hand, if the V content is more than 0.70%, V precipitates will form
even at a temperature equal to or higher than the A
3 point. It is difficult for V precipitates that are formed at a temperature equal
to or higher than the A
3 point to dissolve in the steel, and such V precipitates remain in the steel as insoluble
precipitates. When insoluble precipitates remain, the amount of dissolved V decreases.
Consequently, the temper softening resistance of the steel decreases. In addition,
when insoluble precipitates remain, it is difficult for fine V precipitates to precipitate
by means of a heat treatment conducted thereafter. In such a case, the strength of
the steel decreases. Accordingly, the V content is from 0 to 0.70%. A preferable lower
limit of the V content for stably obtaining the aforementioned effects is 0.05%, and
more preferably is 0.10%. A preferable upper limit of the V content is 0.50%, and
more preferably is 0.30%.
Mo: 0 to 0.70%
[0059] Molybdenum (Mo) is an optional element and need not be contained. If contained, Mo
precipitates as Mo carbides during a heat treatment at a low temperature that is not
more than the A
1, such as a heat treatment for tempering or nitriding. Therefore, the strength and
temper softening resistance of the steel increase. Mo also dissolves in the steel
and increases the hardenability of the steel. The aforementioned effects are obtained
to a certain extent if even a small amount of Mo is contained. On the other hand,
if the Mo content is more than 0.70%, the hardenability of the steel will be too high.
In such a case, a supercooled structure is liable to form during rolling or a softening
heat treatment before wire drawing or the like. Accordingly, the Mo content is from
0 to 0.70%.
[0060] A preferable lower limit of the Mo content for stably obtaining the aforementioned
effects is 0.05%, more preferably is 0.10%, and further preferably is 0.15%. A preferable
upper limit of the Mo content for stably obtaining ferrite, pearlite and bainite in
the micro-structure of the steel is 0.40%, and more preferably is 0.30%.
W: 0 to 0.70%
[0061] Tungsten (W) is an optional element and need not be contained. If contained, W precipitates
as W carbides in the steel and enhances the strength and temper softening resistance
of the steel. W carbides form at a low temperature that is not more than the A
3 point. Therefore, unlike V, Nb, Ti and the like, it is difficult for W to form insoluble
precipitates. Consequently, W carbides increase the strength and temper softening
resistance of the steel by precipitation strengthening. W also dissolves in the steel
and thereby increases the hardenability of the steel and increases the steel strength.
The aforementioned effects are obtained to a certain extent if even a small amount
of W is contained.
[0062] On the other hand, if the W content is more than 0.70%, a supercooled structure is
liable to form, and the hot workability of the steel will thus decrease. Accordingly,
the W content is from 0 to 0.70%. A preferable lower limit of the W content for stably
increasing the temper softening resistance of the steel is 0.05%, and more preferably
is 0.10%. A preferable upper limit of the W content for stably obtaining ferrite,
pearlite and bainite in the micro-structure of the steel is 0.40%, and more preferably
is 0.30%.
[0063] It is difficult for W and Mo to form nitrides. Therefore, these elements can enhance
the temper softening resistance of the steel without being influenced by the N content.
A preferable total content of W and Mo for obtaining a high temper softening resistance
is from 0.10 to 0.30%.
Nb: 0 to less than 0.050%
[0064] Niobium (Nb) is an optional element and need not be contained. If contained, Nb forms
Nb nitrides, Nb carbides, or Nb carbo-nitrides and suppresses coarsening of austenite
grains during quenching or during normalizing. Nb also increases the strength of the
steel by precipitation strengthening. The aforementioned effects are obtained to a
certain extent even if a small amount of Nb is contained. On the other hand, if the
Nb content is more than 0.050%, insoluble precipitates form and the toughness of the
steel decreases. In addition, if the Nb content is more than 0.050%, a supercooled
structure is liable to form and consequently the hot workability of the steel will
decrease. Accordingly, the Nb content is from 0 to less than 0.050%. A preferable
lower limit of the Nb content for stably obtaining the aforementioned effects is 0.001%,
and more preferably is 0.005%. A preferable upper limit of the Nb content is 0.030%,
and more preferably is 0.015%.
Cu: 0 to 0.50%
[0065] Copper (Cu) is an optional element and need not be contained. If contained, Cu prevents
decarburization. Cu also increases corrosion resistance, similarly to Ni. The aforementioned
effects are obtained to a certain extent if even a small amount of Cu is contained.
On the other hand, if the Cu content is more than 0.50%, the steel will become brittle
and rolling defects are liable to arise. Accordingly, the Cu content is from 0 to
0.50%. A preferable lower limit of the Cu content for stably obtaining the aforementioned
effects is 0.05%, and more preferably is 0.10%. In a case where 0.30% or more of Cu
is contained, the hot ductility can be maintained if the Ni content is higher than
the Cu content.
Ti: 0 to 0.100%
[0066] Titanium (Ti) is an optional element and need not be contained. If contained, Ti
forms nitrides, carbides or carbo-nitrides, and suppresses coarsening of austenite
grains during quenching and during normalizing. Ti also increases the strength of
the steel by precipitation strengthening. Ti also deoxidizes the steel. In addition,
in a case where B is contained, Ti combines with dissolved N and maintains the amount
of dissolved B. In this case, the hardenability increases. The aforementioned effects
are obtained to a certain extent if even a small amount of Ti is contained.
[0067] On the other hand, because Ti forms the aforementioned nitrides and sulfides, Ti
influences MnS inclusions and composite inclusions. Specifically, if the Ti content
is more than 0.100%, the crystallized amount of MnS inclusions decreases, and formation
of composite inclusions also decreases. In this case, the rusting characteristics
of the steel decrease. In addition, if the Ti content is too high, the Ti forms nitrides
and sulfides, and the fatigue strength decreases. Accordingly, the Ti content is from
0 to 0.100%. A preferable lower limit of the Ti content for effectively obtaining
the aforementioned effects is 0.003%. In particular, in a case where B is contained,
a preferable lower limit of the Ti content for reducing dissolved N is 0.005%. A preferable
upper limit of the Ti content for increasing corrosion resistance is 0.090%, and more
preferably is 0.080%.
[0068] The steel for machine structural use of the present embodiment may further contain
Ca.
Ca: 0 to 0.0030%
[0069] Calcium (Ca) is an optional element and need not be contained. If contained, Ca forms
CaS or (Mn, Ca)S and spheroidizes MnS inclusions, and reduces the amount of tool wear.
As a result, the machinability of the steel increases. The aforementioned effects
are obtained to a certain extent if even a small amount of Ca is contained. On the
other hand, if the Ca content is more than 0.0030%, oxide-based inclusions coarsen
and the fatigue strength of the steel decreases. Accordingly, the Ca content is from
0 to 0.0030%. A preferable lower limit of the Ca content for further enhancing the
machinability is 0.0001%. When prioritizing fatigue strength over machinability, a
preferable upper limit of the Ca content is 0.0015%, and more preferably is 0.0003%.
[Regarding Formula (1)]
[0070] The chemical composition of the steel for machine structural use of the present embodiment
also satisfies Formula (1).

[0071] Where, a content (mass%) of a corresponding element is substituted for each element
in Formula (1).
[0072] Here, it is defined that F1 = Mn/S. F1 means the Mn content relative to the S content.
If F1 is less than 8.0, it will be difficult for MnS inclusions to adequately crystallize.
Consequently, the amount of dissolved S in the steel after solidification will not
adequately decrease, and a large number of fine MnS precipitates will form after solidification.
In such a case, the rusting characteristics of the steel will decrease because the
total number of MnS inclusions, MnS precipitates, Pb inclusions and composite inclusions
cannot decrease. If the amount of dissolved S in the steel after solidification cannot
be adequately decreased, dissolved S will remain at crystal grain boundaries after
solidification. As a result, in some cases the hot workability of the steel will decrease.
[0073] On the other hand, if F1 is 8.0 or more, the Mn content will be adequately high in
comparison to the S content. In this case, MnS inclusions in the molten steel will
adequately crystallize and grow. As a result, the amount of dissolved S in the steel
after solidification will be adequately decreased, and precipitation of MnS precipitates
in the steel after solidification can be suppressed. Therefore, the total number of
MnS inclusions, MnS precipitates, Pb inclusions and composite inclusions in the steel
can be adequately reduced, and the rusting characteristics of the steel improve. A
preferable lower limit of F1 for improving the rusting characteristics of the steel
is 10.0, and more preferably is 20.0.
[Regarding the steel micro-structure]
[0074] The micro-structure of the steel for machine structural use according to the present
invention is mainly composed of ferrite, pearlite and bainite. Specifically, a total
area fraction of ferrite, pearlite and bainite in the micro-structure of the steel
for machine structural use having the aforementioned chemical composition is 99% or
more.
[0075] The total area fraction of ferrite, pearlite and bainite in the micro-structure can
be measured by the following method. A sample is taken from the steel for machine
structural use. For example, in a case where the steel for machine structural use
is a steel bar or a wire rod, in a transverse section (a face perpendicular to the
axial direction), a sample is taken from a middle part of a radius R (hereunder, referred
to as "R/2 part") that links the external surface and the central axis. Of the entire
area of a transverse section (surface) of the sample of the R/2 part, a surface that
is perpendicular to the central axis of the steel for machine structural use is adopted
as an observation surface. After polishing the observation surface, the observation
surface is subjected to etching using 3% nitric acid-alcohol (nital etching reagent).
The etched observation surface is observed with an optical microscope having a magnification
of ×200, and photographic images of an arbitrary five visual fields are generated.
[0076] In each visual field, the contrast differs for each of the respective phases of ferrite,
pearlite, bainite and the like. Accordingly, the respective phases are identified
based on the contrast. The total area (µm
2) of ferrite, pearlite and bainite among the identified phases is determined for each
visual field. The total area in the respective visual fields is totaled for all of
the visual fields (five visual fields), and the ratio relative to the gross area of
all the visual fields is determined. The determined ratio is defined as the total
area fraction (%) of ferrite, pearlite and bainite.
[Number TN of specific inclusions]
[0077] According to the steel for machine structural use of the present invention, a total
number TN of inclusions (that is, specific inclusions) which are any of MnS inclusions,
Pb inclusions and composite inclusions containing MnS and Pb and which have an equivalent
circular diameter of 5 µm or more in the steel is 40 per mm
2 or more.
[0078] If the number TN of specific inclusions is 40 per mm
2 or more, coarse MnS inclusions having an equivalent circular diameter of 5 µm or
more will adequately crystallize, and as a result the total number of MnS inclusions,
MnS precipitates, Pb inclusions and composite inclusions can be adequately reduced.
Therefore, excellent machinability and excellent rusting characteristics can both
be realized in a compatible manner. On the other hand, if the number TN of specific
inclusions in the steel is less than 40 per mm
2, coarse MnS inclusions having an equivalent circular diameter of 5 µm or more do
not adequately crystallize, and as a result the total number of MnS inclusions, MnS
precipitates, Pb inclusions and composite inclusions cannot be adequately reduced.
Therefore, adequate rusting characteristics are not obtained. A preferable lower limit
of the number TN of specific inclusions is 80 per mm
2, and more preferably is 150 per mm
2. A preferable upper limit of the number TN of specific inclusions is 300 per mm
2. Note that, although an upper limit of the equivalent circular diameter of the specific
inclusions is not particularly limited, for example, the upper limit is 200 µm,
[Ratio of number of composite inclusions among specific inclusions (composite ratio)
RA]
[0079] Preferably, a ratio (hereunder, also referred to as "composite ratio") RA of the
total number (number per mm
2) of composite inclusions having an equivalent circular diameter of 5 µm or more with
respect to the number (number per mm
2) of specific inclusions is 40% or more.
[0080] As described above, the susceptibility of the steel to rusting increases as the total
number of MnS inclusions, MnS precipitates, Pb inclusions and composite inclusions
increases. In this case, the larger the number of composite inclusions that the MnS
inclusions and Pb inclusions form, the more that the total number of MnS inclusions,
MnS precipitates, Pb inclusions and composite inclusions can be reduced. In particular,
the total number of Pb inclusions in the steel can be reduced. Pb inclusions, in particular,
are liable to decrease the rusting characteristics. If the composite ratio is 40%
or more, the total number of MnS inclusions, MnS precipitates, Pb inclusions and composite
inclusions can be reduced, and the number of Pb inclusions that are independently
present can also be reduced. As a result, the rusting characteristics of the steel
can be further enhanced. Accordingly, the composite ratio RA is preferably 40% or
more. In this case, the rusting characteristics of the steel can be further enhanced.
A more preferable lower limit of the composite ratio RA is 60%, and further preferably
is 75%.
[Method of measuring number TN of specific inclusions and composite ratio RA]
[0081] The number TN of specific inclusions and the composite ratio RA can be measured by
the following methods. A sample is taken from the steel for machine structural use
by the method described above. Using a scanning electron microscope (SEM), 20 visual
fields at a transverse section (surface) of the sample of the R/2 part are randomly
observed at a magnification of ×1000. Specific inclusions (any of MnS inclusions,
Pb inclusions and composite inclusions for which an equivalent circular diameter is
5 µm or more) are identified in the respective visual fields (referred to as "observation
surfaces"). It is possible to distinguish specific inclusions and other inclusions
based on contrast. In addition, among the specific inclusions, MnS inclusions, Pb
inclusions and composite inclusions are respectively identified by the following method.
[0082] For each observation surface, an image of the S distribution and Pb distribution
in the observation surface is obtained by means of an X-ray spectroscopy wavelength
dispersion device (EPMA). FIG. 1A is a schematic diagram illustrating the S distribution
in an observation surface, which was obtained by EPMA analysis. FIG. 1B is a schematic
diagram illustrating the Pb distribution in the same observation surface as in FIG.
1A, which was obtained by EPMA analysis.
[0083] Reference numeral 10 in FIG. 1A denotes a region in which S is present. Because S
is almost entirely present as MnS, MnS can be regarded as being present at the locations
indicated by each reference numeral 10 in FIG. 1A. Reference numeral 20 in FIG. 1B
denotes a region in which Pb is present.
[0084] As illustrated in FIG. 1B, in some cases, as shown by reference numeral 20A, Pb is
divided by rolling or the like and is arranged in the rolling direction. The same
applies with respect to S. As illustrated in FIG. 2, in an image obtained by EPMA
analysis, in a case where adjacent inclusions IN each have an equivalent circular
diameter of 5 µm or more, if a distance D between the adjacent inclusions IN is not
more than 10 µm, these inclusions IN are regarded as a single inclusion. Note that,
as described above, the term "equivalent circular diameter" means the diameter of
a circle in a case where the area of the respective inclusions or respective precipitates
is converted into a circle that has the same area. Even when an inclusion group is
defined as a single inclusion, the equivalent circular diameter is the diameter of
a circle having the same total area as the inclusion group.
[0085] FIG. 1C is an image obtained by combining FIG. 1B with FIG. 1A. Referring to FIG.
1C, in the case where the Pb inclusions 20 overlap with the MnS inclusions 10, the
relevant inclusions are recognized as being composite inclusions 30. On the other
hand, referring to FIG. 1C, in the case where the MnS inclusion 10 and the Pb inclusion
20 do not overlap (region A1 and region A2 in FIG. 1C), the relevant inclusions are
identified as an MnS inclusion 10 and a Pb inclusion 20.
[0086] By the above method, MnS inclusions, Pb inclusions and composite inclusions are identified
using a scanning microscope and EPMA. The area of each inclusion that is identified
is determined, and the diameter of a circle with the same area is determined as the
equivalent circular diameter (µm) for each of the inclusions.
[0087] Among the respective inclusions, specific inclusions for which the equivalent circular
diameter is 5 µm or more are identified. The total number (number in 20 visual fields)
of the specific inclusions that are identified is determined, and is converted to
a number TN per mm
2 (inclusions/mm
2). The number TN of specific inclusions is determined by the above method. In addition,
among the identified specific inclusions, a number MN of composite inclusions (inclusions/mm
2) for which the equivalent circular diameter is 5 µm or more is determined, and the
composite ratio RA (%) is determined based on the following Formula (2).

[Production Method]
[0088] An example of a method for producing the steel for machine structural use according
to the present invention will now be described. According to the present embodiment,
a method for producing a steel bar or a wire rod as an example of the steel for machine
structural use will be described. However, a steel for machine structural use according
to the present invention is not limited to a steel bar or a wire rod.
[0089] One example of the production method includes a steel making process of refining
and casting molten steel to produce a starting material (a cast piece or an ingot),
and a hot working process of subjecting the starting material to hot working to produce
a steel for machine structural use. Hereunder, each of these processes is described.
[Steel making process]
[0090] The steel making process includes a refining process and a casting process.
[Refining process]
[0091] In the refining process, firstly, hot metal that was produced by a well-known method
is subjected to refining (primary refining) using a converter. Molten steel that was
tapped from the converter is subjected to secondary refining. In the secondary refining,
an alloy whose components have been adjusted is added to the molten steel to thereby
produce a molten steel having the aforementioned chemical composition.
[0092] Specifically, Mn is added to the molten steel that was tapped from the converter.
As a result, oxides that are mainly composed of Mn form in the molten steel. After
addition of the Mn is completed, Si which has a stronger deoxidizing power than Mn
is added. As a result, the oxides that are mainly composed of Mn are modified to oxides
that are mainly composed of Si. After addition of the Si is completed, Al which has
an even stronger deoxidizing power than Si is added. As a result, the oxides that
are mainly composed of Si are modified to composite oxides containing Si and Al (hereinafter,
also referred to simply as "composite oxides").
[0093] The composite oxides that were formed by the above described refining process serve
as nuclei for crystallization of MnS inclusions. Therefore, by forming the composite
oxides, MnS inclusions adequately crystallize and grow coarse. That is, if composite
oxides form, it is easy for specific inclusions that are inclusions having an equivalent
circular diameter of 5 µm or more to form, and the number TN of specific inclusions
becomes 40 per mm
2 or more. As a result, the amount of dissolved S in the steel after solidification
is adequately reduced, and precipitation of MnS precipitates in the steel after solidification
can be suppressed. Therefore, the total number of MnS inclusions, MnS precipitates,
Pb inclusions and composite inclusions can be adequately reduced, and the rusting
characteristics of the steel are enhanced.
[0094] After deoxidation, slag is removed as well known. After the removing slag, secondary
refining is performed. For example, composite refining is performed as the secondary
refining. For example, first a primary treatment that uses an LF (ladle furnace) or
VAD (vacuum arc degassing) is performed. In addition an RH (Ruhrstahl-Hausen) vacuum
degassing treatment may be performed. In the secondary refining, Mn, Si, and other
elements are added as necessary to adjust the components of the molten steel. After
adjusting the components of the molten steel, a casting process is performed.
[Casting process]
[0095] A starting material (a cast piece or an ingot) is produced using the molten steel
produced by the above described refining process. Specifically, a cast piece is produced
by a continuous casting process using the molten steel. Alternatively, an ingot may
be produced by an ingot-making process using the molten steel. Hereinafter, a cast
piece and an ingot are referred to generically as "starting material". A cross-sectional
area of the starting material in this case is, for example, 200 to 350 mm × 200 to
600 mm.
[0096] A solidification cooling rate RC during casting is 100°C/min or less. If the solidification
cooling rate RC is 100°C/min or less, MnS inclusions adequately crystallize and grow
in the molten steel. Therefore, it is easy for specific inclusions to form, and the
number TN thereof becomes 40 per mm
2 or more. As a result, the amount of dissolved S in the steel after solidification
is adequately reduced, and precipitation of MnS precipitates in the steel after solidification
can be suppressed. Therefore, the total number of MnS inclusions, MnS precipitates,
Pb inclusions and composite inclusions can be adequately reduced, and the rusting
characteristics of the steel are enhanced.
[0097] On the other hand, if the solidification cooling rate RC is more than 100°C/min,
MnS inclusions do not adequately crystallize, and MnS inclusions also do not adequately
grow. Therefore, it will be difficult for specific inclusions to be formed, and the
number TN of specific inclusions will be less than 40 per mm
2. In this case, the amount of dissolved S in the steel after solidification cannot
be adequately reduced, and a large number of fine MnS precipitates will form after
solidification. As a result, since the total number of MnS inclusions, MnS precipitates,
Pb inclusions and composite inclusions cannot be reduced, the rusting characteristics
of the steel will decline. Accordingly, the solidification cooling rate RC is 100°C/min
or less.
[0098] A preferable solidification cooling rate RC is from 8 to less than 50°C/min. In this
case, it is even easier for MnS inclusions to crystallize and grow. Furthermore, if
the solidification cooling rate RC is from 8 to less than 50°C/min, because the time
period until solidifying is long, a sufficient time period for Pb to move through
the molten steel and adhere to MnS inclusions can be secured. Therefore, it is easy
for composite inclusions containing MnS and Pb to form, and the composite ratio RA
becomes 40% or more. A more preferable upper limit of the solidification cooling rate
RC is 30°C/min. A more preferable lower limit of the solidification cooling rate RC
is 10°C/min, and further preferably is 15°C/min.
[0099] The solidification cooling rate RC can be determined based on the starting material
that was cast. FIG. 3 is a transverse sectional view of a starting material that was
cast. In the starting material having a thickness W (mm), at a point PI located at
a position at a depth of W/4 towards the center of the starting material from the
surface, the cooling rate from the liquidus temperature to the solidus temperature
is defined as the solidification cooling rate RC (°C/min) in the casting process.
The solidification cooling rate RC can be determined by the following method. After
solidification, the starting material is cut in the transverse direction. In the transverse
section of the starting material, a secondary dendrite arm spacing λ2 (µm) in the
thickness direction of the solidification structure at the point PI is measured. Using
the measurement value λ2, the solidification cooling rate RC (°C/min) is determined
based on the following Formula (3).

[0100] The secondary dendrite arm spacing λ2 depends on the solidification cooling rate
RC. Accordingly, the solidification cooling rate RC can be determined by measuring
the secondary dendrite arm spacing λ2.
[Hot working process]
[0101] In the hot working process, hot working is usually performed one or a plurality of
times. The starting material is heated before each hot working operation is performed.
Thereafter, the starting material is subjected to the hot working. The hot working
is, for example, hot forging or hot rolling. In the case of performing hot working
a plurality of times, the initial hot working is, for example, blooming or hot forging,
and the next hot working is finish rolling using a continuous mill. In the hot rolling
mill, a horizontal stand having a pair of horizontal rolls, and a vertical stand having
a pair of vertical rolls are alternately arranged in a row. The starting material
after hot working is cooled by a well-known cooling method such as air cooling.
[0102] The steel for machine structural use according to the present embodiment is produced
by the above described processes. The steel for machine structural use is, for example,
a steel bar or a wire rod.
[0103] The steel for machine structural use produced by the above described method is excellent
in machinability and rusting characteristics. Production of the steel for machine
structural use into a machine component is performed, for example, by the following
method.
[0104] The steel for machine structural use is subjected to hot forging to produce an intermediate
product having a rough shape. As necessary, the intermediate product is subjected
to a normalizing. The intermediate product is also subjected to machining. The machining
is, for example, cutting. The intermediate product that underwent machining may be
subjected to a thermal refining treatment (quenching and tempering). In a case where
a thermal refining treatment is performed, the machining such as cutting may be performed
on the intermediate product after the thermal refining treatment. A machine component
is produced by the above process. A machine component may also be produced by performing
cold forging instead of hot forging.
EXAMPLES
[0106] The molten steel of each test number was produced by the following method. Hot metals
produced by a well-known method were subjected to primary refining under the same
conditions using a converter to thereby produce the molten steels of the respective
test numbers.
[0107] For the molten steels of test numbers other than Test Numbers 48 and 49, after tapping
the molten steel from the converter, Mn, Si and Al were added in that order to perform
deoxidation. For the molten steel of Test Number 48, after tapping the molten steel
from the converter, Si, Al and Mn were added in that order to perform deoxidation.
For the molten steel of Test Number 49, after tapping the molten steel from the converter,
Mn, Al and Si were added in that order to perform deoxidation.
[0108] After the deoxidation, slag is removed. After removing slag, a primary treatment
was performed using VAD, and thereafter an RH vacuum degassing treatment was performed.
After the RH vacuum degassing treatment, final adjustment of alloying elements was
performed. Molten steels having the chemical compositions shown in Table 1 were produced
by the above described process.
[0109] Each of the molten steels was cast to produce an ingot for test use that had a rectangular
parallelepiped shape. The cross sectional shape of the ingot was a rectangular shape
with dimensions of 190 mm × 190 mm. The solidification cooling rates RC (°C/min) for
the respective test numbers were as listed in Table 2. The solidification cooling
rate RC was determined by measuring a secondary dendrite arm spacing of the ingot
and applying the determined value to the aforementioned Formula (3).
[Table 2]
| Test Number |
Deoxidation Order |
RC (°C/min) |
F1= Mn/S |
Micro-structure |
TN (inclusions/mm2) |
RA (%) |
Rusting Characteristics |
Machinability |
Rolling Contact Fatigue Life (hours) |
Overall Evaluation |
| CL1000 (m/min) |
Chip Treatability |
| 1 |
Mn→Si→Al |
46.0 |
17.0 |
F+P+B |
136.5 |
73.1 |
⊙ |
57 |
○ |
4.5 |
○ |
| 2 |
Mn→Si→Al |
41.9 |
9.1 |
F+P+B |
84.8 |
87.1 |
⊙ |
60 |
○ |
3.1 |
○ |
| 3 |
Mn→Si→Al |
37.9 |
72.9 |
F+P+B |
42.2 |
84.8 |
⊙ |
52 |
○ |
5.0 |
○ |
| 4 |
Mn→Si→Al |
15.0 |
36.1 |
F+P+B |
119.0 |
77.7 |
⊙ |
46 |
○ |
4.0 |
○ |
| 5 |
Mn→Si→Al |
27.1 |
13.7 |
F+P+B |
190.7 |
73.2 |
⊙ |
45 |
○ |
3.3 |
○ |
| 6 |
Mn→Si→Al |
46.5 |
19.3 |
F+P+B |
52.9 |
74.8 |
⊙ |
53 |
○ |
5.7 |
○ |
| 7 |
Mn→Si→Al |
84.7 |
27.1 |
F+P+B |
48.9 |
31.2 |
○ |
46 |
○ |
4.6 |
○ |
| 8 |
Mn→Si→Al |
94.8 |
59.6 |
F+P+B |
68.7 |
39.3 |
○ |
48 |
○ |
3.1 |
○ |
| 9 |
Mn→Si→Al |
65.8 |
19.4 |
F+P+B |
58.9 |
35.9 |
○ |
51 |
○ |
4.5 |
○ |
| 10 |
Mn→Si→Al |
76.9 |
46.3 |
F+P+B |
121.3 |
20.1 |
○ |
52 |
○ |
4.4 |
○ |
| 11 |
Mn→Si→Al |
74.3 |
15.5 |
F+P+B |
42.7 |
33.6 |
○ |
51 |
○ |
3.2 |
○ |
| 12 |
Mn→Si→Al |
76.5 |
9.6 |
F+P+B |
70.9 |
33.7 |
○ |
55 |
○ |
5.1 |
○ |
| 13 |
Mn→Si→Al |
55.9 |
18.9 |
F+P+B |
102.6 |
37.6 |
○ |
49 |
○ |
6.4 |
○ |
| 14 |
Mn→Si→Al |
65.3 |
31.0 |
F+P+B |
51.6 |
29.0 |
○ |
43 |
○ |
6.6 |
○ |
| 15 |
Mn→Si→Al |
71.6 |
12.9 |
F+P+B |
80.2 |
31.7 |
○ |
49 |
○ |
4.8 |
○ |
| 16 |
Mn→Si→Al |
59.5 |
13.4 |
F+P+B |
154.4 |
34.5 |
○ |
60 |
○ |
5.7 |
○ |
| 17 |
Mn→Si→Al |
72.2 |
27.6 |
F+P+B |
71.5 |
22.1 |
○ |
47 |
○ |
4.1 |
○ |
| 18 |
Mn→Si→Al |
69.1 |
20.2 |
F+P+B |
73.8 |
38.9 |
○ |
53 |
○ |
6.1 |
○ |
| 19 |
Mn→Si→Al |
63.8 |
10.7 |
F+P+B |
91.6 |
32.7 |
○ |
40 |
○ |
4.4 |
○ |
| 20 |
Mn→Si→Al |
15.9 |
18.3 |
F+P+B |
68.8 |
63.6 |
⊙ |
45 |
○ |
4.2 |
○ |
| 21 |
Mn→Si→Al |
51.6 |
14.5 |
F+P+B |
86.5 |
33.4 |
○ |
49 |
○ |
6.2 |
○ |
| 22 |
Mn→Si→Al |
80.6 |
28.8 |
F+P+B |
58.6 |
32.8 |
○ |
47 |
○ |
4.3 |
○ |
| 23 |
Mn→Si→Al |
91.4 |
13.1 |
F+P+B |
91.9 |
32.4 |
○ |
45 |
○ |
6.6 |
○ |
| 24 |
Mn→Si→Al |
42.8 |
22.8 |
F+P+B |
61.7 |
56.6 |
⊙ |
57 |
○ |
6.8 |
○ |
| 25 |
Mn→Si→Al |
55.8 |
20.3 |
F+P+B |
112.5 |
38.6 |
○ |
41 |
○ |
5.9 |
○ |
| 26 |
Mn→Si→Al |
55.9 |
27.1 |
F+P+B |
66.1 |
38.3 |
○ |
48 |
○ |
6.2 |
○ |
| 27 |
Mn→Si→Al |
69.1 |
12.9 |
F+P+B |
91.2 |
32.2 |
○ |
45 |
○ |
6.2 |
○ |
| 28 |
Mn→Si→Al |
143.7 |
27.6 |
F+P+B |
19.8 |
22.2 |
× |
47 |
○ |
4.7 |
× |
| 29 |
Mn→Si→Al |
184.7 |
17.5 |
F+P+B |
39.9 |
27.0 |
× |
44 |
○ |
6.7 |
× |
| 30 |
Mn→Si→Al |
188.0 |
14.1 |
F+P+B |
33.0 |
34.4 |
× |
50 |
○ |
3.4 |
× |
| 31 |
Mn→Si→Al |
121.6 |
19.9 |
F+P+B |
38.9 |
29.9 |
× |
51 |
○ |
6.9 |
× |
| 32 |
Mn→Si→Al |
100.9 |
14.5 |
F+P+B |
33.6 |
33.6 |
× |
51 |
○ |
4.6 |
× |
| 33 |
Mn→Si→Al |
114.1 |
20.0 |
F+P+B |
32.0 |
28.4 |
× |
54 |
○ |
6.3 |
× |
| 34 |
Mn→Si→Al |
193.5 |
26.9 |
F+P+B |
37.0 |
39.6 |
× |
45 |
○ |
4.4 |
× |
| 35 |
Mn→Si→Al |
159.6 |
20.9 |
F+P+B |
38.9 |
23.0 |
× |
42 |
○ |
6.0 |
× |
| 36 |
Mn→Si→Al |
135.2 |
13.5 |
F+P+B |
32.3 |
27.7 |
× |
44 |
○ |
6.4 |
× |
| 37 |
Mn→Si→Al |
22.8 |
6.0 |
F+P+B |
31.0 |
39.2 |
× |
46 |
○ |
4.9 |
× |
| 38 |
Mn→Si→Al |
76.0 |
7.5 |
F+P+B |
38.4 |
30.5 |
× |
48 |
○ |
4.1 |
× |
| 39 |
Mn→Si→Al |
126.7 |
7.3 |
F+P+B |
36.3 |
34.8 |
× |
51 |
○ |
4.5 |
× |
| 40 |
Mn→Si→Al |
88.1 |
49.3 |
F+P+B |
69.0 |
74.8 |
⊙ |
26 |
○ |
5.3 |
× |
| 41 |
Mn→Si→Al |
23.8 |
15.0 |
F+P+B |
23.9 |
30.2 |
× |
42 |
○ |
3.8 |
× |
| 42 |
Mn→Si→Al |
40.9 |
229.4 |
F+P+B |
44.5 |
31.8 |
× |
41 |
○ |
5.0 |
× |
| 43 |
Mn→Si→Al |
181.1 |
26.1 |
F+P+B |
105.6 |
33.8 |
× |
43 |
○ |
6.2 |
× |
| 44 |
Mn→Si→Al |
11.9 |
27.2 |
F+P+B |
52.4 |
75.1 |
⊙ |
35 |
× |
4.3 |
× |
| 45 |
Mn→Si→Al |
56.7 |
37.7 |
F+P+B |
37.1 |
34.1 |
× |
55 |
○ |
5.2 |
× |
| 46 |
Mn→Si→Al |
24.1 |
24.8 |
F+P+B |
82.1 |
63.9 |
⊙ |
32 |
○ |
6.1 |
× |
| 47 |
Mn→Si→Al |
23.3 |
23.2 |
F+P+B |
92.2 |
72.6 |
⊙ |
52 |
○ |
1.7 |
× |
| 48 |
Si→Al→Mn |
46.2 |
22.8 |
F+P+B |
36.2 |
29.9 |
× |
52 |
○ |
6.2 |
× |
| 49 |
Mn→Al→Si |
48.6 |
22.8 |
F+P+B |
37.1 |
31.8 |
× |
56 |
○ |
6.1 |
× |
[0110] The produced ingots for test use were subjected to hot working twice to produce a
steel bar. In the hot working, blooming was performed, and thereafter finish rolling
(steel bar rolling) was performed. The produced test ingot was subjected to hot forging
to produce a steel bar having a diameter of 50 mm. Alternatively, the test ingot was
subjected to blooming, and then subjected to finish rolling to produce a steel bar
having a diameter of 50 mm. A normalizing treatment in a range of 800 to 950°C was
performed on the produced steel bar. The cooling method adopted in the normalizing
treatment was to allow cooling of the steel bar. A steel bar (steel for machine structural
use) having a diameter of 50 mm was produced by the above-described production process.
[Evaluation tests]
[Micro-structure observation]
[0111] A test specimen for micro-structure observation use was taken from the R/2 part of
the steel bar of each test number. Of the entire surface of the test specimen, a cross-section
parallel to the longitudinal direction (that is, the rolling direction or elongation
direction) of the steel bar was defined as the observation surface. The total area
fraction (%) of ferrite, pearlite and bainite were determined based on the method
described above. The total area fraction was 99% or more in the micro-structure of
the steel bar of each test number. A micro-structure in which the total area fraction
was 99% or more is shown as "F+P+B" in Table 2.
[Number TN of specific inclusions and composite ratio RA]
[0112] A test specimen for observing the micro-structure was taken from the R/2 part of
the steel bar of each test number. Of the entire surface of the test specimen, a cross-section
that was parallel to the longitudinal direction (that is, the rolling direction or
elongation direction) of the steel bar was defined as the observation surface. For
the observation surface of the test specimen for observing the micro-structure of
each test number, the specific inclusions number TN (inclusions/mm
2) and the composite ratio RA (%) were determined based on the above described method.
The results are shown in Table 2.
[Machinability]
[0113] A service life characteristic in the case of normal drilling, and the chip treatability
were evaluated with respect to the machinability.
[Service life characteristic CL1000]
[0114] The steel bar having a diameter of 50 mm was cut at a length of 20 mm to make a piercing
test specimen. The piercing test specimen was subjected to piercing. The piercing
conditions are shown in Table 3.
[Table 3]
| Cutting Speed |
10-70 m/min |
| Feed Rate |
0.25 mm/rev |
| Wet Type |
Water-soluble Cutting Oil |
| Drill |
Diameter |
3 mm |
| Point Angle |
118° |
| Material |
High-speed Steel Straight Drill |
| Other |
Hole Depth |
9 mm |
| Service Life |
Until Breakage |
[0115] Specifically, the cumulative hole depth was measured up to drill breakage at different
peripheral speeds of the drill. A high-speed steel straight drill was used as the
drill. The nose radius of the drill was 3 mm, and the point angle was 118°. Piercing
was performed at a cutting speed of 10 to 70 m/min, a feed rate of 0.25 mm/rev, and
a hole depth of 9 mm. Piercing with one drill was ended when the cumulative hole depth
(hole depth × number of piercings) reached 1000 mm. In such case, the drill was replaced,
and the peripheral speed of the drill was raised to a higher speed and the test was
repeated until drill breakage. The maximum peripheral speed of the drill at which
it was possible to pierce a cumulative hole depth of 1000 mm was defined as CL1000
(m/min), and the CL1000 value was adopted as an index of the machinability. The results
are shown in the "CL1000" column in Table 2. In a case where CL1000 was 40 m/min or
more, the service life characteristic was determined as being excellent. On the other
hand, when CL1000 was less than 40 m/min, the service life characteristic was determined
as being not excellent.
[Chip treatability evaluation]
[0116] A steel bar having a diameter of 50 mm was cut to a predetermined length and adopted
as a cutting test specimen. Outer circumferential lathe turning shown in FIG. 4 was
performed on the cutting test specimen. The conditions for the outer circumferential
lathe turning are shown in Table 4.
[Table 4]
| Cutting Speed |
250 m/min |
| Depth-of-cut Amount |
2 mm |
| Feed Rate |
0.2 mm/rev |
| Wet Type |
Water-soluble Cutting Oil |
| Tool |
Chip |
P20 Cemented Carbide Tool |
| SNMG 120408 Circumference Groove With Breaker |
| Holder |
DSBN-R2525 |
[0117] Specifically, a P20 cemented carbide tool was used as a tool 50. The nose radius
of the tool 50 was 0.4, and the rake angle thereof was 5°. Outer circumferential lathe
turning was performed under the following conditions: cutting speed V1: 250 m/min;
feed speed V2: 0.2 mm/rev; depth-of-cut amount D1: 2 mm; and longitudinal direction
cutting length L1: 200 mm. After cutting the outer circumference, cutting lathe turning
was repeated again so as to obtain a small diameter of D1: 2 mm, and with respect
to test specimen 5, a lathe turning test was performed under the aforementioned conditions
for four minutes.
[0118] In the lathe turning for the 1000
th test specimen, a chip as illustrated in FIG. 5A and FIG. 5B was obtained. A length
L20 and a diameter D20 of the chip were measured. Based on the measurement result,
the chip treatability was evaluated as follows. If the diameter D20 of the chip was
a coil shape of not more than 30 mm, or if the chip length L20 was less than 50 mm
even if the chip was not a coil shape, the chip treatability was determined as being
excellent ("○" in Table 2). On the other hand, if the diameter D20 of the chip was
not a coil shape of not more than 30 mm, and the chip length L20 was also 50 mm or
more, the chip treatability was determined as being not excellent ("×" in Table 2).
[Rusting characteristics (corrosion resistance) evaluation test]
[0119] A rust test specimen was prepared by cutting the steel bar having a diameter of 50
mm to a predetermined length. The rust test specimen was subjected to lathe turning
under similar conditions as in the aforementioned cutting test. Thereafter, the test
specimen was stored for one hour in an atmosphere with a humidity of 70% and a temperature
of 20°C while spraying tap water onto the cut surface. After storage, the cut surface
of the test specimen was observed and the number of rust points was measured. The
measurement results are shown in the "rusting characteristics" column in Table 2.
If the number of rust points was less than 10 (indicated by "⊙" in Table 2), and if
the number of rust points was 10 or more and less than 20 (indicated by "○" in Table
2), the rusting characteristics were determined as being excellent. On the other hand,
if the number of rust points was 20 or more ("×" in Table 2), the rusting characteristics
were determined as being not excellent.
[Rolling contact fatigue test]
[0120] Evaluation of the rolling contact fatigue life was performed by means of a Mori thrust-type
rolling contact fatigue test. Ten disk-shaped rolling contact fatigue test specimens
100 having a diameter of 60 mm and a thickness of 5 mm as illustrated in FIG. 6 were
taken from the R/2 part of the steel bar of each test number. Each rolling contact
fatigue test specimen 100 was subjected to quenching and tempering to harden the surface
thereof. The effective hardened layer depth was made 0.8 mm or more.
[0121] The quenching and tempering treatment conditions were as follows: 880°C × 1 hour,
oil quenching, washing and low-temperature tempering at 170°C × 2 hours. The surface
of each test specimen on which the quenching and tempering treatment was performed
was subjected to grinding, and the effective hardened layer depth was made 0.5 mm.
The depth from the surface to a position at which the hardness became HV550 was adopted
as the effective hardened layer depth. The amount removed by grinding was set to about
0.1 mm. The hardness distribution and effective hardened layer depth in each test
specimen were adjusted by adjusting the Cp and the grinding removal amount.
[0122] As illustrated in FIG. 7, each rolling contact fatigue test specimen 100 was immersed
in lubricating oil 102 composed of 70% oil and 30% water, and because the moisture
in the lubricating oil evaporated due to heat generation, 30 ml of water was added
once per day. The test interfacial pressure was set to a constant pressure of 4 kN.
The hard balls that were used were Si
3N
4 ceramic hard balls. Three hard balls were placed in contact with the top of the rolling
contact fatigue test specimen 100, and the number of revolutions was set to 1200 rpm.
As a measure of the rolling contact fatigue life, "time (hours) until producing pitting
at a cumulative failure probability of 10% obtained when the test result was plotted
on Weibull probability paper" was used as the durable life. The results are shown
in the "rolling contact fatigue life" column in Table 2. In a case where the rolling
contact fatigue life was 3.1 hours or more, the rolling contact fatigue properties
were determined as being excellent. On the other hand, if the rolling contact fatigue
life was less than 3.1 hours, the rolling contact fatigue properties were determined
as being not excellent.
[Test results]
[0123] In Test Numbers 1 to 27, the chemical composition was appropriate, F1 was 8.0 or
more, the deoxidation order was appropriate, and the solidification cooling rate RC
was 100°C/min or less. Therefore, the number TN of specific inclusions was 40 per
mm
2 or more. As a result, CL1000 was 40 m/min or more, and excellent chip treatability
was obtained. That is, excellent machinability was obtained. In addition, in the rusting
characteristics evaluation test, the number of rust points was less than 20 for each
of these test numbers, and thus excellent rusting characteristics were obtained. Furthermore,
in the rolling contact fatigue test, for each of these test numbers, the rolling contact
fatigue life was 3.1 hours or more, and thus excellent rolling contact fatigue properties
were obtained.
[0124] Furthermore, in Test Numbers 1 to 6, 20 and 24, the solidification cooling rate RC
was in a range of 8 to less than 50°C/min. Therefore, not only was the number TN of
specific inclusions 40 per mm
2 or more, but furthermore the composite ratio RA was 40% or more. As a result, for
each of these test numbers, the number of rust points was less than 10, and thus rusting
characteristics that were even more excellent in comparison to Test Numbers 7 to 19,
21 to 23, and 25 to 27 were obtained.
[0125] On the other hand, in Test Numbers 28 to 36, although the chemical composition was
appropriate and F1 was 8.0 or more and the deoxidation order was appropriate, the
solidification cooling rate RC was more than 100°C/min. Consequently, the number TN
of specific inclusions was less than 40 per mm
2. As a result, excellent rusting characteristics were not obtained.
[0126] In Test Numbers 37 and 38, although the chemical composition was appropriate and
the deoxidation order was appropriate and the solidification cooling rate RC was not
more than 100°C/min, F1 was less than 8.0. Consequently, the number TN of specific
inclusions was less than 40 per mm
2. As a result, excellent rusting characteristics were not obtained.
[0127] In Test Number 39, although the chemical composition was appropriate and the deoxidation
order was appropriate, the solidification cooling rate RC was more than 100°C/min
and F1 was less than 8.0. Consequently, the number TN of specific inclusions was less
than 40 per mm
2. As a result, excellent rusting characteristics were not obtained.
[0128] In Test Number 40, the Mn content was too high. As a result, CL1000 was less than
40 m/min, and thus excellent machinability was not obtained.
[0129] In Test Number 41, the Mn content was too low. Consequently, the number TN of specific
inclusions was less than 40 per mm
2. As a result, excellent rusting characteristics were not obtained.
[0130] In Test Number 42, the S content was too low. As a result, excellent rusting characteristics
were not obtained.
[0131] In Test Number 43, the Pb content was too high. In addition, the solidification cooling
rate RC was more than 100°C/min. As a result, excellent rusting characteristics were
not obtained.
[0132] In Test Number 44, the Pb content was too low. As a result, CL1000 was less than
40 m/min and, furthermore, excellent chip treatability was not obtained. That is,
excellent machinability was not obtained.
[0133] In Test Number 45, the Al content was too low. Consequently, the number TN of specific
inclusions was less than 40 per mm
2. As a result, excellent rusting characteristics were not obtained.
[0134] In Test Number 46, the Cr content was too high. As a result, CL1000 was less than
40 m/min, and thus excellent machinability was not obtained.
[0135] In Test Number 47, the Cr content was too low. As a result, the rolling contact fatigue
life was less than 3.1 hours, and thus excellent rolling contact fatigue properties
were not obtained.
[0136] In Test Numbers 48 and 49, although the chemical composition was appropriate, F1
was 8.0 or more and the solidification cooling rate RC was not more than 100°C/min,
the deoxidation order was inappropriate. Consequently, the number TN of specific inclusions
was less than 40 per mm
2. As a result, excellent rusting characteristics were not obtained.
[0137] An embodiment of the present invention has been described above. However, the foregoing
embodiment is merely an example for implementing the present invention. Accordingly,
the present invention is not limited to the above embodiment, and the above embodiment
can be appropriately modified within a range which does not deviate from the gist
of the present invention.
REFERENCE SIGNS LIST
[0138]
- 10
- MnS Inclusions
- 20
- Pb Inclusions
- 30
- Composite Inclusions