BACKGROUND OF THE INVENTION
Field of the Invention
[0001] The present invention relates to an aluminum alloy which shows low friction characteristics.
It is suitable for use as engine components of automobiles and is excellent in both
tensile strength and wear resistance.
Description of the Related Art
[0002] An aluminum alloy has light weight and excellent processability. So it has been conventionally
used as structural materials of air planes and automobiles. Recently, an engine of
automobiles comes to require high power and low fuel consumption. In accordance with
this requirement, the aluminum alloy is being applied for rocker arms, shift forks
and engine components such as piston or cylinder head. So, the aluminum alloy is improved
in its wear resistance and tensile strength.
[0003] Al-based composite materials having excellent wear resistance and excellent stiffness
include, for example, a high tensile aluminum alloy material. It is produced by powder
metallurgy in which particles, whiskers and fibers of SiC or Al₂O₃ are added into
Al-Cu-Mg alloy (2000 series) or Al-Mg-Si alloy (6000 series).
[0004] A high tensile aluminum alloy powder having excellent tensile strength, excellent
wear resistance and low thermal expansion is developed (See Japanese Patent Publication
No. 56401/1990). The method for producing the high tensile aluminum alloy powder is
that 7.7 to 15% of Ni is added to an Al-Si alloy, then Cu and Mg are added. Concerning
the obtained high tensile aluminum alloy powder, the size of primary Si is less than
15µm.
[0005] Regarding piston, a skirt portion requires excellent wear resistance, excellent heat
conductivity, low thermal expansion and excellent tensile strength. Cylinder liner
requires excellent wear resistance, excellent antiseize and low friction coefficient.
[0006] The above alloy such as 2000 series alloy or 6000 series alloy is used as matrix,
and particles, whiskers and fibers of SiC or Al₂O₃ are added into the matrix, thereby
obtaining Al-based Metal Matrix Composites (hereinafter described as MMC). It shows
poor tensile strength because the matrix itself shows poor tensile strength.
[0007] When the above Al-based MMC is used as a sliding member of the above piston or the
above cylinder liner, the temperature of a sliding portion rises. So, agglutination
abrasion or abrasive friction generates, and friction coefficient becomes high and
abrasion loss becomes large. Therefore, to use the Al-based MMC as the sliding member
is restricted not only at high temperature but also room temperature.
[0008] The above high tensile aluminum alloy in which Ni is added into an Al-Si alloy shows
excellent tensile strength because stable Al-Ni intermetallic compounds are formed.
When the high tensile aluminum alloy is used as a sliding member, it shows poor wear
resistance since hard particles such as ceramics are not included. Concerning sliding
characteristics, Al is adhered to the mating member because of agglutination. The
high tensile aluminum alloy cannot be improved in its friction coefficient, seize
load and abrasion loss. Therefore, the high tensile aluminum alloy is used as the
sliding member only for the restricted area under the restricted condition.
[0009] When the conventional aluminum alloy is used as the sliding member of the engine
component, it shows poor tensile strength and poor sliding characteristics.
SUMMARY OF THE INVENTION
[0010] Concerning the above problems, it is an object of the present invention to provide
an aluminum alloy which shows excellent tensile strength and excellent sliding characteristics
(i.e. excellent wear resistance and excellent antiseize in spite of low friction).
[0011] Inventors examined a base composition for the purpose of obtaining tensile strength
and wear resistance of the matrix. As the result, we happened to think that wear resistance
is obtained by precipitating primary Si crystal within the range of hyper-eutectic
of an Al-Si alloy. Similarly, we also happened to think that tensile strength is obtained
by adding Ni and Cu.
[0012] Concerning the above matrix, inventors further studied a dispersant for the purpose
of improving sliding characteristics. As the result, we found the following facts.
When nitride is dispersed, Al is not adhered to the mating member, and wear resistance
and antiseize are obtained with low friction coefficient. When boride is dispersed,
fluid lubrication of B₂O₃ occurs, and wear resistance and antiseize are obtained in
spite of low friction coefficient. When oxide or carbide is dispersed, wear resistance
improves. Therefore, inventors completed the present invention.
[0013] An aluminum alloy according to the present invention is excellent in its tensile
strength and wear resistance. The aluminum alloy consists essentially of 90 to 99.5%
by weight of matrix and 0.5 to 10% by weight of a dispersant dispersed within the
matrix. The matrix comprises 10 to 25% by weight of Si, 5 to 20% by weight of Ni,
1 to 5% by weight of Cu and the rest of Al and impurity elements. The dispersant is
one selected from the group consisting of 0.5 to 10% of nitride, boride, carbide and
oxide.
[0014] The amount of Si is in the range of 10 to 25%. Regarding a hyper-eutectic Al-Si alloy,
Si is dispersed as primary crystal and eutectic, so tensile strength and wear resistance
improve. When the amount of Si is less than 10%, the Al-Si alloy is hypo-eutectic,
and it has α phase + eutectic structure. In this case, tensile strength and wear resistance
are not expected. When the amount of Si is more than 25%, Si particle as primary crystal
becomes large even if powder metallurgy is used. In this case, the mating member is
attacked, and machinability in producing becomes remarkably bad. Furthermore, elongation
of the material is very small, and the crack is produced in processing. So, the aluminum
alloy in this case is not suitable for practical use.
[0015] The amount of Ni is in the range of 5 to 20%. Intermetallic compounds such as Al₃Ni
are formed in the aluminum alloy by using Ni. These intermetallic compounds are stable
even at high temperature, and they are useful for tensile strength and wear resistance.
When the amount of Ni is less than 5%, the intermetallic compounds of Al-Ni is not
formed. So, tensile strength and wear resistance cannot be obtained. When the amount
of Ni is more than 20%, tensile strength and wear resistance are excellent. On the
other hand, machinability deteriorates, so the aluminum alloy in this case is not
suitable for practical use.
[0016] The amount of Cu is in the range of 1 to 5%. Cu is useful for improving tensile strength
of the aluminum alloy. When the amount of Cu is less than 1%, tensile strength is
weak. When the amount of Cu is more than 5%, coarse CuAl₂ particle is produced, so
strength is weak.
[0017] The Al-Si alloy as matrix has hyper-eutectic structure because the amount of Si is
10 to 25%. Fine primary Si crystal is formed, so excellent wear resistance is provided.
Since the Al-Si alloy also contains 5 to 20% of Ni, the intermetallic compounds such
as Al₃Ni or Al₃Ni₂ are formed. Therefore, tensile strength and wear resistance improve.
Furthermore, tensile strength improves because 1 to 5% of Cu is added. Figure 7 shows
X-ray diffraction result of Al-15Ni-15Si-3Cu, and Al₃Ni and Al₃Ni₂ are produced.
[0018] The amount of nitride is in the range of 0.5 to 10%. When nitride is dispersed into
the matrix, friction coefficient is lowered, and antiseize and wear resistance improve.
Furthermore, Al isn't adhered to the mating member, and it can slide easily. When
the amount of nitride is less than 0.5%, the above-described effect cannot be obtained.
When the amount of nitride is more than 10%, flexural tensile strength and ductility
deteriorate. So, desirable amount of nitride is 0.5 to 10%.
[0019] The amount of boride is in the range of 0.5 to 10%. When boride is dispersed into
the matrix, B₂O₃ is produced by oxidation of B because TiB₂ is thermodynamically unstable.
The melting point of B₂O₃ is 450°C. The part of B₂O₃ changes to liquid, and finally
becomes liquid lubrication. So, friction coefficient of the aluminum alloy is lowered,
and antiseize and wear resistance improve. When the amount of boride is less than
0.5%, the above-described effect cannot be obtained. When the amount of boride is
more than 10%, mechanical property such as flexural strength and ductility is remarkably
lowered. So, desirable amount of boride is 0.5 to 10%.
[0020] The amount of carbide or oxide is in the range of 0.5 to 10%. The hardness of carbide
or oxide is in the range of Hv1500 to 3000. For example, Al₂O₃ is Hv2050, NbO is Hv1900,
SiO₂ is Hv1700, SiC is Hv2200, B₄C is Hv2350 and VC is Hv2500. When these elements
are dispersed into the matrix, wear resistance improves. When the amount of carbide
or oxide is less than 0.5%, the above-described effect cannot be obtained. When the
amount of carbide or oxide is more than 10%, mechanical property such as flexural
strength and ductility is remarkably lowered. So, desirable amount of carbide or oxide
is 0.5 to 10%.
[0021] The above nitride includes, for example, AlN, TiN, ZrN, Cr₂N and BN. The above boride
includes, for example, TiB₂, NiB, MgB₂ and ZrB₂. The above carbide includes, for example,
Cr₃C₂, B₄C, ZrC, SiC and VC. The above oxide includes, for example, Al₂O₃, NbO, SiO₂,
MgO and Cr₂O₃. The dispersant is in a form of powders, whiskers and fibers.
[0022] The above dispersant is dispersed into the matrix by means of powder metallurgy.
At first, the dispersant is mixed within the aluminum alloy powder. Then, the obtained
mixed powder is sintered, forged, extruded and rolled. Finally, the mixed powder become
solid and compacting is obtained.
[0023] Though there is no limit to particle diameter of the dispersant, desirable particle
diameter is in the range of 0.2 to 20µm. When the particle diameter is less than 0.2µm,
the powder is agglomerated, and mechanical characteristics deteriorates. When the
particle diameter is more than 20µm, the particle is cracked or omitted at the time
of sliding. Then, abrasive friction occurs, and the effect of wear resistance is weakened.
[0024] When nitride is dispersed into the matrix, Al is not adhered to the mating member
and it can easily be slided. So, not only low friction coefficient but also antiseize
and excellent wear resistance can be obtained. When boride is dispersed into the matrix,
B₂O₃ having low melting point is produced on the sliding surface. Since boride performs
liquid lubrication, low friction coefficient, wear resistance and antiseize improve.
When carbide or oxide is dispersed into the matrix, wear resistance improves. This
is why carbide or oxide has a hardness of Hv1500 to 3000.
BRIEF DESCRIPTION OF THE DRAWINGS
[0025] A more complete appreciation of the present invention and many of its advantages
will be readily obtained as the same becomes better understood by reference to the
following detailed description when considered in connection with the accompanying
drawings and detailed specification, all of which forms a part of the disclosure:
[0026] Figure 1 is a cross sectional view of a test piece and a mating member which are
used for friction experiment.
[0027] Figure 2 is a cross sectional view for showing friction experiment.
[0028] Figure 3 is an EPMA photograph (magnification x 1000) for showing Al distribution
on the surface of the mating member when LFW experiment is performed on the example
of the present invention in which AlN is dispersed .
[0029] Figure 4 is an EPMA photograph (magnification x 1000) for showing Al distribution
on the surface of the mating member when LFW experiment is performed on the comparative
example in which AlN is not dispersed.
[0030] Figure 5 is a SEM photograph (magnification x 1000) after LFW experiment is performed
on the example of the present invention in which AlN is dispersed.
[0031] Figure 6 is an EPMA photograph (magnification x 1000) for showing N distribution
when LFW experiment is performed on the example of the present invention in which
AlN is dispersed.
[0032] Figure 7 shows X-ray diffraction result of Al-15Ni-15Si-3Cu.
[0033] Figure 8 are optical micrographs (magnification x 100 and 400) for showing the metal
structure of the comparative example 9.
[0034] Figure 9 are optical micrographs (magnification x 100 and 400) for showing the metal
structure of the example 1 of the present invention.
[0035] Figure 10 are optical micrographs (magnification x 100 and 400) for showing the metal
structure of the example 2 of the present invention.
[0036] Figure 11 is a SEM photograph (magnification x 5000) for showing the appearance of
the dispersed AlN particle in the preferred embodiments.
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS
[0037] Having generally described the present invention, a further understanding can be
obtained by reference to the specific preferred embodiments which are provided herein
for purposes of illustration only and are not intended to limit the scope of the appended
claims.
[0038] The Preferred Embodiments according to the present invention will be hereinafter
described with reference to Figures 1 through 11.
[0039] In the Preferred Embodiment, an alloy containing Al, 15% of Si, 15% of Ni and 3%
of Cu was melted and atomized, thereby obtaining an aluminum alloy powder. The aluminum
alloy powder was classified by 100 mesh sieve, and -100 mesh powder was obtained.
The average particle diameter was D₅₀ = 33µm. As compared with the above-mentioned
aluminum alloy powder, an alloy containing Al, 4.5 % of Cu, 1.6% of Mg and 0.5% of
Mn (being equivalent to AA 2024) was used, and -100 mesh powder was obtained. Similarly,
when an alloy containing Al, 1.0% of Mg, 0.6% of Si and 0.3% of Cu (being equivalent
to AA 6061) was used, -100 mesh powder was obtained.
[0040] The above aluminum alloy powder was mixed with nitride such as AlN, TiN or ZrN, boride
such as TiB₂, NiB or MgB₂, carbide such as SiCp, SiCw or B₄Cp, and oxide such as Al₂O₃p
or B₂O₃p in a grinding machine. Concerning nitride, boride, carbide and oxide, the
adding amount and the average particle diameter were shown in Table 1.
[0041] The mixed powder was filled within a tube made of pure Al. Then a vacuum degassing
was performed, and the tube was sealed. After that, the temperature of the tube was
heated to 450°C, and the tube having the mixed powder therein was extruded at extrusion
ratio of 10. Finally, the extruded material was mechanically processed. Concerning
the extruded material, tensile strength, abrasion loss, friction coefficient and seize
load were measured. The results were shown in Table 2.

[0042] The friction coefficient and seize load were measured by a testing machine as shown
in Figure 1. A ring-shaped member 1, JIS SUJ2, was pressed against a box-shaped test
piece 2 under the condition that a load was increased by 250(N) and a sliding speed
was 13m/min. Then, friction coefficient and seize load were measured under a drying
condition. The abrasion loss was measured by LFW testing machine as shown in Figure
2. A ring-shaped member 4, JIS SUJ2, was immersed into oil 3. Then, a box-shaped test
piece 5 was pressed against the ring-shaped member 4 under the condition that the
load was 150(N) and the sliding speed was 18m/min. After being pressed for 15 minutes,
abrasion loss was measured.
[0043] Concerning comparative examples 9, 19 and 20 in Table 2, a matrix comprised the aluminum
alloy only, and the dispersant wasn't dispersed. These comparative examples 9, 19
and 20 showed excellent tensile strength, and the values of tensile strength were
in the range of 385 to 440MPa at 200°C. But the comparative example 9 showed rather
high friction coefficient, and the value of friction coefficient was 0.48. According
to friction coefficient, the value of seize load was about 1000(N). Since the dispersant
wasn't dispersed, the values of abrasion loss were in the range of 43 to 65µm. The
comparative examples 9, 19 and 20 showed poor wear resistance.
[0044] Concerning comparative example 10, the composition of the matrix was AA 2024, and
SiC was dispersed in more amount than that was needed. The comparative example 10
showed poor tensile strength, and the tensile strength at 200°C was 170MPa. Moreover,
the comparative example 10 showed rather high friction coefficient, and the value
of friction coefficient was 0.53. According to friction coefficient, the value of
seize load was 1000(N). Furthermore, the value of abrasion loss was 45µm. The comparative
example 10 showed poor tensile strength, poor antiseize, and poor wear resistance.
[0045] Concerning comparative example 11, the composition of the matrix was AA 6061, and
SiC was dispersed in more amount than that was needed. The comparative example 11
showed poor tensile strength, and the tensile strength at 200°C was 210MPa. Moreover,
the comparative example 11 showed rather high friction coefficient, and the value
of friction coefficient was 0.58. According to friction coefficient, the value of
seize load was 750(N). Furthermore, the value of abrasion loss was 48µm. The comparative
example 11 showed poor tensile strength, poor antiseize, and poor wear resistance.
[0046] On the contrary, examples 1 to 8 and 12 to 15 showed excellent tensile strength,
excellent antiseize, and excellent wear resistance. The examples 1 to 8 and 12 to
15 showed excellent tensile strength, and the tensile strength at 200°C were in the
range of 400 to 520MPa. The examples 4 to 6 in which SiC and Al₂O₃ were dispersed
showed a little bit higher friction coefficient and lower seize load. However, the
examples 1 to 3, 7 and 8 showed lower friction coefficient and excellent seize load,
and the values of friction coefficient were in the range of 0.35 to 0.38, and the
values of seize load were in the range of 1500 to 1750(N). The examples 1 and 2 in
which AlN was dispersed showed very excellent abrasion loss, and the values of abrasion
loss were in the range of 2 to 3µm. Similarly, as for the examples 16 to 18, the values
of abrasion loss were in the range of 3 to 9µm. Moreover, the examples 3 to 8 also
showed excellent abrasion loss, and the values of abrasion loss were in the range
of 23 to 35µm. Especially, the examples 12 to 15 in which nitride and boride are dispersed
showed more excellent wear resistance as compared with examples in which oxide and
carbide are dispersed.
[0047] Figure 3 is an EPMA photograph (magnification x 1000) for showing Al distribution
on the surface of the ring-shaped member when LFW experiment is performed on the example
1 of the present invention in which AlN is dispersed. According to Figure 3, Al is
hardly adhered to the ring-shaped member. On the contrary, Figure 4 shows that Al
is adhered to the ring-shaped member and agglutination abrasion is occured. Figure
4 is an EPMA photograph (magnification x 1000) for showing Al distribution on the
surface of the ring-shaped member when LFW experiment is performed on the comparative
example 9 in which AlN is not dispersed.
[0048] Figure 5 is a SEM photograph (magnification x 1000) after LFW experiment is performed
on the example 1 of the present invention in which AlN is dispersed. Figure 6 is an
EPMA photograph (magnification x 1000) for showing N distribution after LFW experiment
is performed on the example 1 of the present invention in which AlN is dispersed.
As is obvious from Figures 5 and 6, it is confirmed that AlN particle is held in the
matrix after LFW experiment is performed. It is also confirmed that no AlN particle
is omitted.
[0049] Figure 8 (a) and (b) are optical micrographs (magnification x 100 and 400) for showing
the metal structure of the comparative example 9. Figure 9 (a) and (b) are optical
micrographs (magnification x 100 and 400) for showing the metal structure of the example
1. Figure 10 (a) and (b) are optical micrographs (magnification x 100 and 400) for
showing the metal structure of the example 2. As is obvious from these optical micrographs,
in the examples 1 and 2, it is confirmed that AlN particle is held in the matrix after
LFW experiment is performed. It is also confirmed that no AlN particle is omitted.
Figure 11 is a SEM photograph (magnification x 5000) for showing the appearance of
the dispersed AlN particle in the preferred embodiments.
[0050] As above-described, the present invention completed an aluminum alloy which shows
excellent tensile strength and excellent wear resistance. The aluminum alloy consists
essentially of 90 to 99.5% by weight of matrix and 0.5 to 10% by weight of a dispersant
dispersed within the matrix. The matrix comprises 10 to 25% by weight of Si, 5 to
20% by weight of Ni, 1 to 5% by weight of Cu and the rest of Al and impurity elements.
The dispersant is one selected from the-group consisting of 0.5 to 10% of nitride,
boride, carbide and oxide. The Al-Si alloy as matrix has hyper-eutectic structure
because the amount of Si is 10 to 25%. Excellent wear resistance is provided by fine
primary Si crystal. Since the Al-Si alloy also contains 5 to 20% of Ni, intermetallic
compounds such as Al₃Ni or Al₃Ni₂ are formed. Therefore, tensile strength and wear
resistance improve. Furthermore, tensile strength improves because 1 to 5% of Cu is
added.
[0051] When nitride is dispersed into the matrix, Al is not adhered to the ring-shaped member
and it can easily slide. So, not only low friction coefficient but also antiseize
and excellent wear resistance can be obtained. When boride is dispersed into the matrix,
liquid phase B₂O₃ having low melting point is produced on the sliding surface. Since
boride performs liquid lubrication, low friction coefficient, wear resistance and
antiseize improve. When carbide or oxide is dispersed into the matrix, wear resistance
improves. This is why carbide or oxide has a very high hardness of Hv1 500 to 3000.
[0052] As the result, the obtained aluminum alloy member can be applied to engine parts,
an intake valve, a piston, or the like. This achieves light weight of these elements.
The aluminum alloy shows high-heat conductivity and it is excellent in its tensile
strength and wear resistance. Therefore, the aluminum alloy is suitable for the intake
valve, and it is applied to the piston of high power engine. Furthermore, the aluminum
alloy is also applied to cylinder liner since it is excellent in its wear resistance
and antiseize. Moreover, when the aluminum alloy is applied to a valve retainer or
a spring retainer, this achieves light weight of their elements.
1. An aluminum alloy consisting essentially of 90 to 99.5% by weight of matrix and 0.5
to 10% by weight of a dispersant dispersed within said matrix, said matrix comprising
10 to 25% by weight of Si, 5 to 20% by weight of Ni, 1 to 5% by weight of Cu and the
rest of Al and impurity elements, said dispersant being at least one selected from
the group consisting of 0.5 to 10% of nitride, boride, carbide and oxide.
2. An aluminum alloy according to claim 1, wherein said nitride is AlN, TiN, ZrN, Cr₂N
or BN.
3. An aluminum alloy according to claim 1, wherein said boride is TiB₂, NiB, MgB₂ or
ZrB₂.
4. An aluminum alloy according to claim 1, wherein said carbide is Cr₃C₂, B₄C, ZrC, SiC
or VC.
5. An aluminum alloy according to claim 1, wherein said oxide is Al₂O₃, NbO, SiO₂, MgO
or Cr₂O₃.
6. An aluminum alloy according to claim 1, wherein said dispersant is in a form of powders,
whiskers or fibers.
7. An aluminum alloy according to claim 1, wherein said dispersant is in a form of powders
of which the diameter is in the range of 0.2 to 20µm.
8. An aluminum alloy according to claim 1, wherein said dispersant is dispersed into
the matrix by means of powder metallurgy.
9. An aluminum alloy according to claim 1, wherein the tensile strength at 200°C is in
the range of 400 to 490MPa.