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IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308
_______________________________________________________________________________________
Volume: 04 Issue: 04 | Apr-2015, Available @ http://www.ijret.org 593
WEAR CHARACTERISTICS OF PURE ALUMINIUM, AL-ALLOY &
AL-ALUMINA METAL MTRIX NANO COMPOSITE IN DRY
CONDITION: PART-I
Vyjainto Kumar Ray1
, Payodhar Padhi2
, B. B. Jha3
, Tapas Kumar Sahoo4
1
Student of Ph.D., Mechanical Engineering Department, B.P.U.T., Bhubaneswar, Orissa, India
2
Principal, Mechanical Engineering Department, K.I.S.T., Bhubaneswar, Orissa, India
3
Chief Scientist, Metallurgical Engineering, Surface engineering department, I.M.M.T., Bhubaneswar, Orissa, India
4
Technical Assistant, Metallurgical Engineering, Surface engineering department, I.M.M.T., Bhubaneswar, Orissa,
India
Abstract
In this report, an aluminium metal matrix was reinforced with 1.5 wt. % of Al2O3 nano particles using non-contact cavitation
method to prepare the metal matrix nano composite. Microstructural examination conducted on the sample revealed a uniform
distribution of alumina particulates. Sliding wear behavior of the as-cast MMNC was studied in dry condition, under different test
conditions by varying the load and the sliding velocity, with an unlubricated Multiple Tribo Tester. It was found that sliding wear
resistance improved considerably with the addition of alumina nano particles. Microscopic examinations of the worn out surfaces
of pure Al, Al-alloy (duralumin) and MMNC reveal that the MMNC has greater resistance to sliding wear compared to pure
aluminium and duralumin. Wear increases with increase in load and sliding velocity. Delamination and abrasion are the
dominating types of wear observed.
Keywords: Sliding Wear, Al2O3, MMNC, Duralumin, Delamination and Abrasion.
--------------------------------------------------------------------***----------------------------------------------------------------------
1. INTRODUCTION
With the development of new processing techniques and the
demand for lighter materials with high strength and
stiffness, high performance composite materials have been
developed which show enhanced properties compared to
traditional metals and alloys. Most of these high
performance materials are metallic matrixes reinforced with
fibre, particulate or whiskers. MMNCs are emerging as the
most versatile materials for advanced structural, automotive,
aviation, aerospace, defense applications because of their
excellent combination of properties. In recent years,
considerable interest has been paid in extending the use of
these composite materials in marine environment [1, 2].
These MMNCs have emerged as the important class of
advanced materials giving the prospect to tailor the material
properties according to their needs. These materials differ
from the conventional engineering materials because of their
homogeneity [3]. Aluminium based MMNCs possess
desirable properties like high specific stiffness, low density,
high specific strength controlled co efficient of thermal
expansion, increased fatigue resistance and superior
dimensional stability at elevated temperatures etc. [4, 5].
The mechanical and tribological properties of the MMNCs
can be improved by reinforcing various materials ranging
from very soft materials like Graphite, Talc etc. to high
hardened ceramic particulates like SiC, Al2O3, etc., [6, 7].
However, because of their high cost of production, their
application in industries is slowed down. Casting
Technology plays the key to overcome this problem,
although several technical challenges exist. Achieving a
uniform distribution of reinforcement within the matrix is a
big challenge, which directly influences the properties and
quality of the composite materials. The MMNCs possess
excellent mechanical and tribological properties and are,
therefore, considered as prospective engineering materials
for various tribological applications [8-15]. It is reported by
many researchers that sliding wear resistance and abrasion
resistance of MMCs and MMNCs, reinforced with ceramic
particulates like SiC, Al2O3, have improved [8-11]. When
nano particles of quantity as small as 2 wt. percent are
added, it enhances the hardness and yield strength by a
factor as high as 2 [16]. There are several methods for the
production of metal matrix nano composites which include
mechanical alloying, vertex process, and spray deposition
etc. But, the above processes are expensive. Solidification
processing is a relatively cheaper route. Nano particulates
tend to agglomerate during solidification processing as a
result of Van der Waals forces and therefore, proper
dispersion of the nano particulates in metal matrix is a
challenge. In the present work, a non-contact method, where
the ultrasonic probe is not in direct contact with the liquid
metal, was attempted to disperse nano sized Al2O3
particulates in aluminum matrix. In this method, the mold
was subjected to ultrasonic vibration [16-20].
But, no work has ever been reported on the dry sliding wear
behavior of MMNCs produced by non-contact cavitation
method [16, 21]. Therefore, in the present investigation, an
attempt has been made to study the dry sliding wear
IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308
_______________________________________________________________________________________
Volume: 04 Issue: 04 | Apr-2015, Available @ http://www.ijret.org 594
behavior of Al+1.5% by wt. Al2O3 MMNC, prepared by
non-contact cavitation method, under different test
conditions by varying applying loads and sliding speeds
over a predefined time period.
2. EXPERIMENTAL PROCEDURE
2.1 Material
Alumina is a high hardened ceramic material. The chemical
composition of the composite (Al-Al2O3 1.5% by wt. nano
particle) is shown in Table 1. The motto to design MMNC is
to combine the metals & ceramic i.e. addition of high
strength, high modulus refractory particles to ductile metal
matrix to get tailor made properties.
Table 1. Composition of Al-Al2O3 (1.5 wt. %) MMNC
Element Fe Mg Si Al Al2O3
Wt. % 1.3 0.43 0.26 96.51 1.5
Fig-1. HRTEM micrograph of Al2O3 nano powder
The Nano composites are prepared by a non-contact
ultrasonic solidification method by Padhi et al [16, 21].
2.2 Preparation of MMNC
The procedure for preparation of MMNC done by Padhi et
al [16, 21] is as follows. The experimental set up is shown in
Fig.1. It consists of an ultrasonic generator that generates
ultrasonic waves, an ultrasonic chamber and steel mould.
The mould was preheated to avoid thermal cracking. The
preheated mould was kept in the ultrasonic chamber and the
chamber was subjected to vibration at a frequency of 35
KHz. Liquid aluminum and alumina particulate (1.5 wt. %)
having average size 10 nm were simultaneously poured into
the vibrating mould from the mixing chamber.
Fig-2: Experimental set up
After the simultaneous pouring, the heating element was
immediately brought down above the liquid metal in order
to delay the solidification. The vibration was carried out for
a period of five minutes to ensure complete mixing. The
castings were obtained in both longitudinal and transverse
section.
Fig-3: HRTEM micrographs of Al-Al2O3 nano composite
showing uniform distribution of nano particles
2.3 Wear Tests
The experiments described here were carried out on a
Multiple Tribo Tester (TR-5), Ducom make. In this Multiple
Tribo Tester, the wheel rotates and the specimen, of size
6.35 x 6.35 x 9 mm, is pressed against the wheel .The
specimen is held by the fixture. Loads ranging from 0 to
1000 N and speeds up to 2000 rpm can be applied to press
the specimen against the periphery of the 20 mm thick, 60
mm diameter wheel. Since the specimen is held stationary
and the wheel rotates, the sliding contact occurs between the
wheel and the specimen and wear of both takes place as the
load is applied for the predefined test duration. Here, the
sliding wear tests were carried out under different load
conditions and at different speeds for a period of 30 minutes
or 1800 seconds. The test conditions are as follows.
1. Constant load of 100 N, constant speed of 300 rpm and
test duration of 30 minutes (1800 seconds).
IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308
_______________________________________________________________________________________
Volume: 04 Issue: 04 | Apr-2015, Available @ http://www.ijret.org 595
2. Constant load of 100 N, constant speed of 350 rpm and
test duration of 30 minutes (1800 seconds).
3. Constant load of 130 N, constant speed of 300 rpm and
test duration of 30 minutes (1800 seconds).
3. RESULTS AND DISCUSSION
The aluminum, duralumin and MMNC specimens were
subjected to the above said test conditions. Duralumin is an
aluminum-copper alloy. In addition to aluminium, the main
materials constituting duralumin are copper, manganese and
magnesium. It is used in aviation and automobile industry.
Fig-4: Wear verses time keeping load (100 N) constant at
two different speeds 300 and 350 rpm for pure aluminium,
duralumin (Al-alloy) and MMNCs.
Fig 4 shows the graph between wear in (µm) verses time in
seconds for pure aluminium, duralumin and MMNC keeping
load constant i.e. 100N, at two different speeds of 300 and
350 rpm. The sliding wear of commercially pure aluminium
in both the conditions shows that under 100N load and 300
& 350 rpm, the wear increases w.r.t. time in both the cases.
But when speed increases to 350 rpm from 300 rpm within a
short span of time i.e. 300 seconds, the material gets
completely worn out. In case of duralumin, as it is harder
than pure aluminium, it covers the total time duration i.e.
1800 seconds under 100N and 300 rpm, but registers more
wear compared to MMNC. When speed goes up to 350 rpm,
it gets complete worn out within 800 seconds. Further, in
case of MMNC, in both the cases, though rpm varies from
300 to 350 rpm, no significant variation in the time occurs.
Also the maximum wear under 300 rpm, in case of MMNC
is 300 µm which occurs after 1800 seconds whereas, in case
of duralumin it is 500 µm after 1800 seconds and in case of
pure aluminium, it is 1500 µm at 900 seconds
approximately. When speed increases to 350 rpm, the wear
in case of pure aluminium increases to 2300 µm and the
complete worn out takes place at 300 seconds.
Hence it is concluded that the wear properties of MMNC is
significantly increased compared to both alloy pure
aluminium.
Fig-5: Wear verses time keeping speed constant (300 rpm)
at two different loads 100 and 130 N for pure Al, duralumin
and MMNC.
Fig. 5 shows the wear verses time keeping speed constant at
300 rpm under 100 N and 130 N load. It is observed that
wear of MMNCs increases gradually and linearly (under
100N) as time increases up to 1800 seconds. But when load
increases from 100N to 130 N, wear increases to 600 µm
(under 130N) from 300 µm (under 100N) suddenly and then
remains nearly constant up to 1800 seconds. In both the load
conditions, MMNC covers 1800 seconds. In case of
duralumin, the wear is 500 µm under 100N load covering
1800 seconds and 2000 µm under 130N load covering only
300 seconds, whereas, in case of pure aluminium, the wear
increases to 1400 µm under 100N load covering 900 sec and
1200 µm under 130 N load covering 600 seconds. This
happens because of bonding of nano particles embedded in
the aluminium matrix uniformly.
Fig-6: Weight loss verses sliding distance under constant
load (100 N) at two different speeds 300rpm and 350 rpm
for pure Al, duralumin and MMNC.
Figure 6 shows weight loss verses sliding distance keeping
load constant at two different speeds. Weight loss for
MMNC at 100N is nearly zero at 300 and 350 rpm though
IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308
_______________________________________________________________________________________
Volume: 04 Issue: 04 | Apr-2015, Available @ http://www.ijret.org 596
there is a little difference which is not so significant where
as in case of duralumin, wt. loss rises first within few meters
of sliding distance and then becomes uniform over the
whole sliding distance. When speed increases to 350 rpm,
initially wt. loss rises severely and then falls and continues
almost uniformly up to 900 meters of sliding distance. For
duralumin, wt. loss is significantly varying under both the
conditions. In case of pure aluminium, when rpm varies
from 300 rpm to 350 rpm, weight loss of material varies
significantly as shown. Initially the material is sticking to
the wheel which indicates negative.
Fig-7: Weight loss verses sliding distance keeping speed
constant (300 rpm) at two different loads 100 and 130 N for
pure Al, duralumin and MMNC.
Figure 7 shows weight loss verses sliding distance keeping
speed constant at two different loads. Weight loss for
MMNC at 300 rpm is nearly zero at100N and 130N rpm
though there is a little difference which is not so significant
whereas in case of both duralumin and pure aluminium,
when load varies from 100N to 130N, weight loss of
material varies significantly as shown. Initially duralumin
and pure aluminium is sticking to the wheel which indicates
negative.
Fig-8: Force of friction verses time keeping load (100 N)
constant at two different speeds 300 and 350 rpm for
MMNC, duralumin and pure aluminium.
The characteristic curves between force of friction and time
for pure aluminium, duralumin and MMNC specimens with
constant load of 100N and at two different speeds of 300
and 350 rpm are shown in Fig 8. For MMNC in both the
conditions, the force of friction is constant over the entire
time period of 1800 seconds. When speed rises to 350 rpm
from 300 rpm, the force of friction reduces. In case of pure
aluminium, force of friction is zero under both he speeds of
300 rpm and 350 rpm. As the material is sticking to the
wheel, the characteristic curves in both the cases show
negative throughout 900 seconds (under 100 N) and 300
seconds (under 130 N) of time periods they covered
respectively. At 300 rpm, in case of duralumin, the force of
friction curve is uniform throughout the entire sliding
distance of 1800 seconds with little frictional resistance
whereas under 350 rpm, the alloy material is sticking to the
wheel for which the characteristic curve shows negative
throughout 800 seconds of time period it covered. Friction is
more in case of MMNC compared to pure Al and alloy and
hence, resistance to wear is more in case of MMNC.
Fig-9: Force of friction verses time keeping speed constant
(300 rpm) at two different loads 100 and 130 N for pure Al,
duralumin and MMNC.
The characteristic curves between force of friction and time
for pure aluminium, duralumin and MMNC specimens with
constant speed of 300 rpm and at two different loads of 100
N and 130 N are shown in Fig 9. For MMNC, at 100 N, the
coeff. of friction is constant over the entire time period of
1800 seconds and at 130 N, the curve initially rises and then
reduces and moves almost uniformly over the entire time
period of 1800 seconds. When load rises to 130 N, the force
of friction reduces. In case of duralumin, under 100 N load,
the curve is uniform over the entire time period, but when
load rises to 130 N, the material is sticking to the wheel and
hence, the characteristic curve shows negative. It covers
only 300 seconds. In case of pure aluminium, force of
friction is zero under both 100 N and 130 N. As the material
is sticking to the wheel, the characteristic curves show
negative throughout 900 seconds (under 100 N) and 600
seconds (under 130 N) of time periods respectively. Friction
is more in case of MMNC specimen compared to pure Al
and alloy.
IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308
_______________________________________________________________________________________
Volume: 04 Issue: 04 | Apr-2015, Available @ http://www.ijret.org 597
4. MICROSCOPIC EVALUATION
The microstructure of the worn out samples were evaluated
under FESEM. The FESEM images are shown in the figures
below.
Fig-10 Microstructure of pure Al at 100N and 300 rpm Fig-11 Microstructure of alloy at 100N and 300 rpm
Fig-12 Microstructure of MMNC at 100N and 300 rpm Fig. 13 Microstructure of pure Al at 100N and 350 rpm
IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308
_______________________________________________________________________________________
Volume: 04 Issue: 04 | Apr-2015, Available @ http://www.ijret.org 598
Fig. 14 Microstructure of alloy at 100N and 350 rpm Fig. 15 Microstructure of MMNC at 100N and 350 rpm
Fig. 16 Microstructure of pure Al at 130N and 300 rpm Fig. 17 Microstructure of alloy at 130N and 300 rpm
Fig. 18 Microstructure of MMNC at 130N and 300 rpm
IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308
_______________________________________________________________________________________
Volume: 04 Issue: 04 | Apr-2015, Available @ http://www.ijret.org 599
Figure 10, 11 and 12 show the FESEM micrographs of worn
out surfaces of pure aluminium, alloy and MMNC
respectively. From the worn out surface of pure Al in figure
10, a nodular surface is observed due to heat generation and
localized welding. The metal worn out becomes more
because of the sticky surfaces. From the worn out
microstructure of alloy shown in fig. 11, scratches are
observed and the microstructure is not that smooth for which
the wear is more than MMNC. From the worn out surface of
MMNC in figure 12, the morphology of worn out
microstructure is nearly smooth because of which wear rate
is almost negligible keeping wear constant.
Figure 13, 14 and 15 show the FESEM images of worn out
samples at 100N load and 350 rpm of pure aluminium, alloy
and composite respectively. Figure 13 shows an irregular
honey comb structure because of ploughing action whereas
fig. 14 shows deep scratches on the surface of alloy because
of rise in speed and figure 15 has smooth microstructure
showing worn out surface of MMNC uniform. But if the
FESEM of fig. 12 is compared with that of fig. 15, wear in
this case is found to be more.
Similarly when load increases to 130 N, the FESEM shown
in figure 16, 17 and 18 show the severe wear in case of pure
aluminium and alloy compared to composite. This happens
due to strengthening mechanism of the nano particles
embedded in the matrix. Since particles are very small and
when embedded in the matrix, no projections are coming out
of the surfaces. Hence, no ploughing action takes place thus
keeping the wear uniform in case of MMNC.
The average surface roughness value of pure Al, alloy and
MMNC are Ra 10.5 µm, Ra 4.2 µm and Ra 5.04 µm
respectively under 100 N load and 300 rpm speed. Similarly,
it is Ra 8.4 µm, Ra 5.0 µm and Ra 6.52 µm for pure Al,
alloy and MMNC respectively under 100 N load and 350
rpm speed. Again, it is Ra 3.0 µm, Ra 5.2 µm and 3.8 µm
for pure Al, alloy and MMNC respectively under 130 N load
and 300 rpm speed.
5. CONCLUSION
As this paper reports the dry sliding wear behaviour of pure
aluminium, alloy and MMNC, the following conclusions
can be drawn.
(a) Wear decreases as the time duration increases.
(b) Wear increases with the increase in load.
(c) Wear increases with the increase in speed.
(d) Force of friction reduces with rise in load and
speed.
The results shown by MMNC are encouraging in
comparison to pure aluminium and duralumin as far as wear,
material loss and friction are concerned. This is because of
the strengthening mechanism due to uniform dispersion of
Al2O3 nano particles in the matrix. Addition of nano
alumina powder to aluminium increases the mechanical and
tribological properties of MMNC. It also improves the
hardness, yield strength, wear and abrasion resistance of the
composite [24]. Again this is light in weight.
FUTURE SCOPE
More tests are required to study all the parameters varying
the load, speed, time as well as weight percentage of
reinforcements. MMNCs can be prepared by varying the
weight percentage of alumina and by reinforcing alumina in
the matrix of duralumin. Even hybrid MMNCs can be
prepared using non-contact ultrasonic cavitation method and
tribological properties can be studied.
REFERENCE
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IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308
_______________________________________________________________________________________
Volume: 04 Issue: 04 | Apr-2015, Available @ http://www.ijret.org 600
[14]. A.P. Sannino and H.J. Rack, ―Dry Sliding Wear of
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Wear Characteristics of Al-Al2O3 MMNC in Dry Condition

  • 1. IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308 _______________________________________________________________________________________ Volume: 04 Issue: 04 | Apr-2015, Available @ http://www.ijret.org 593 WEAR CHARACTERISTICS OF PURE ALUMINIUM, AL-ALLOY & AL-ALUMINA METAL MTRIX NANO COMPOSITE IN DRY CONDITION: PART-I Vyjainto Kumar Ray1 , Payodhar Padhi2 , B. B. Jha3 , Tapas Kumar Sahoo4 1 Student of Ph.D., Mechanical Engineering Department, B.P.U.T., Bhubaneswar, Orissa, India 2 Principal, Mechanical Engineering Department, K.I.S.T., Bhubaneswar, Orissa, India 3 Chief Scientist, Metallurgical Engineering, Surface engineering department, I.M.M.T., Bhubaneswar, Orissa, India 4 Technical Assistant, Metallurgical Engineering, Surface engineering department, I.M.M.T., Bhubaneswar, Orissa, India Abstract In this report, an aluminium metal matrix was reinforced with 1.5 wt. % of Al2O3 nano particles using non-contact cavitation method to prepare the metal matrix nano composite. Microstructural examination conducted on the sample revealed a uniform distribution of alumina particulates. Sliding wear behavior of the as-cast MMNC was studied in dry condition, under different test conditions by varying the load and the sliding velocity, with an unlubricated Multiple Tribo Tester. It was found that sliding wear resistance improved considerably with the addition of alumina nano particles. Microscopic examinations of the worn out surfaces of pure Al, Al-alloy (duralumin) and MMNC reveal that the MMNC has greater resistance to sliding wear compared to pure aluminium and duralumin. Wear increases with increase in load and sliding velocity. Delamination and abrasion are the dominating types of wear observed. Keywords: Sliding Wear, Al2O3, MMNC, Duralumin, Delamination and Abrasion. --------------------------------------------------------------------***---------------------------------------------------------------------- 1. INTRODUCTION With the development of new processing techniques and the demand for lighter materials with high strength and stiffness, high performance composite materials have been developed which show enhanced properties compared to traditional metals and alloys. Most of these high performance materials are metallic matrixes reinforced with fibre, particulate or whiskers. MMNCs are emerging as the most versatile materials for advanced structural, automotive, aviation, aerospace, defense applications because of their excellent combination of properties. In recent years, considerable interest has been paid in extending the use of these composite materials in marine environment [1, 2]. These MMNCs have emerged as the important class of advanced materials giving the prospect to tailor the material properties according to their needs. These materials differ from the conventional engineering materials because of their homogeneity [3]. Aluminium based MMNCs possess desirable properties like high specific stiffness, low density, high specific strength controlled co efficient of thermal expansion, increased fatigue resistance and superior dimensional stability at elevated temperatures etc. [4, 5]. The mechanical and tribological properties of the MMNCs can be improved by reinforcing various materials ranging from very soft materials like Graphite, Talc etc. to high hardened ceramic particulates like SiC, Al2O3, etc., [6, 7]. However, because of their high cost of production, their application in industries is slowed down. Casting Technology plays the key to overcome this problem, although several technical challenges exist. Achieving a uniform distribution of reinforcement within the matrix is a big challenge, which directly influences the properties and quality of the composite materials. The MMNCs possess excellent mechanical and tribological properties and are, therefore, considered as prospective engineering materials for various tribological applications [8-15]. It is reported by many researchers that sliding wear resistance and abrasion resistance of MMCs and MMNCs, reinforced with ceramic particulates like SiC, Al2O3, have improved [8-11]. When nano particles of quantity as small as 2 wt. percent are added, it enhances the hardness and yield strength by a factor as high as 2 [16]. There are several methods for the production of metal matrix nano composites which include mechanical alloying, vertex process, and spray deposition etc. But, the above processes are expensive. Solidification processing is a relatively cheaper route. Nano particulates tend to agglomerate during solidification processing as a result of Van der Waals forces and therefore, proper dispersion of the nano particulates in metal matrix is a challenge. In the present work, a non-contact method, where the ultrasonic probe is not in direct contact with the liquid metal, was attempted to disperse nano sized Al2O3 particulates in aluminum matrix. In this method, the mold was subjected to ultrasonic vibration [16-20]. But, no work has ever been reported on the dry sliding wear behavior of MMNCs produced by non-contact cavitation method [16, 21]. Therefore, in the present investigation, an attempt has been made to study the dry sliding wear
  • 2. IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308 _______________________________________________________________________________________ Volume: 04 Issue: 04 | Apr-2015, Available @ http://www.ijret.org 594 behavior of Al+1.5% by wt. Al2O3 MMNC, prepared by non-contact cavitation method, under different test conditions by varying applying loads and sliding speeds over a predefined time period. 2. EXPERIMENTAL PROCEDURE 2.1 Material Alumina is a high hardened ceramic material. The chemical composition of the composite (Al-Al2O3 1.5% by wt. nano particle) is shown in Table 1. The motto to design MMNC is to combine the metals & ceramic i.e. addition of high strength, high modulus refractory particles to ductile metal matrix to get tailor made properties. Table 1. Composition of Al-Al2O3 (1.5 wt. %) MMNC Element Fe Mg Si Al Al2O3 Wt. % 1.3 0.43 0.26 96.51 1.5 Fig-1. HRTEM micrograph of Al2O3 nano powder The Nano composites are prepared by a non-contact ultrasonic solidification method by Padhi et al [16, 21]. 2.2 Preparation of MMNC The procedure for preparation of MMNC done by Padhi et al [16, 21] is as follows. The experimental set up is shown in Fig.1. It consists of an ultrasonic generator that generates ultrasonic waves, an ultrasonic chamber and steel mould. The mould was preheated to avoid thermal cracking. The preheated mould was kept in the ultrasonic chamber and the chamber was subjected to vibration at a frequency of 35 KHz. Liquid aluminum and alumina particulate (1.5 wt. %) having average size 10 nm were simultaneously poured into the vibrating mould from the mixing chamber. Fig-2: Experimental set up After the simultaneous pouring, the heating element was immediately brought down above the liquid metal in order to delay the solidification. The vibration was carried out for a period of five minutes to ensure complete mixing. The castings were obtained in both longitudinal and transverse section. Fig-3: HRTEM micrographs of Al-Al2O3 nano composite showing uniform distribution of nano particles 2.3 Wear Tests The experiments described here were carried out on a Multiple Tribo Tester (TR-5), Ducom make. In this Multiple Tribo Tester, the wheel rotates and the specimen, of size 6.35 x 6.35 x 9 mm, is pressed against the wheel .The specimen is held by the fixture. Loads ranging from 0 to 1000 N and speeds up to 2000 rpm can be applied to press the specimen against the periphery of the 20 mm thick, 60 mm diameter wheel. Since the specimen is held stationary and the wheel rotates, the sliding contact occurs between the wheel and the specimen and wear of both takes place as the load is applied for the predefined test duration. Here, the sliding wear tests were carried out under different load conditions and at different speeds for a period of 30 minutes or 1800 seconds. The test conditions are as follows. 1. Constant load of 100 N, constant speed of 300 rpm and test duration of 30 minutes (1800 seconds).
  • 3. IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308 _______________________________________________________________________________________ Volume: 04 Issue: 04 | Apr-2015, Available @ http://www.ijret.org 595 2. Constant load of 100 N, constant speed of 350 rpm and test duration of 30 minutes (1800 seconds). 3. Constant load of 130 N, constant speed of 300 rpm and test duration of 30 minutes (1800 seconds). 3. RESULTS AND DISCUSSION The aluminum, duralumin and MMNC specimens were subjected to the above said test conditions. Duralumin is an aluminum-copper alloy. In addition to aluminium, the main materials constituting duralumin are copper, manganese and magnesium. It is used in aviation and automobile industry. Fig-4: Wear verses time keeping load (100 N) constant at two different speeds 300 and 350 rpm for pure aluminium, duralumin (Al-alloy) and MMNCs. Fig 4 shows the graph between wear in (µm) verses time in seconds for pure aluminium, duralumin and MMNC keeping load constant i.e. 100N, at two different speeds of 300 and 350 rpm. The sliding wear of commercially pure aluminium in both the conditions shows that under 100N load and 300 & 350 rpm, the wear increases w.r.t. time in both the cases. But when speed increases to 350 rpm from 300 rpm within a short span of time i.e. 300 seconds, the material gets completely worn out. In case of duralumin, as it is harder than pure aluminium, it covers the total time duration i.e. 1800 seconds under 100N and 300 rpm, but registers more wear compared to MMNC. When speed goes up to 350 rpm, it gets complete worn out within 800 seconds. Further, in case of MMNC, in both the cases, though rpm varies from 300 to 350 rpm, no significant variation in the time occurs. Also the maximum wear under 300 rpm, in case of MMNC is 300 µm which occurs after 1800 seconds whereas, in case of duralumin it is 500 µm after 1800 seconds and in case of pure aluminium, it is 1500 µm at 900 seconds approximately. When speed increases to 350 rpm, the wear in case of pure aluminium increases to 2300 µm and the complete worn out takes place at 300 seconds. Hence it is concluded that the wear properties of MMNC is significantly increased compared to both alloy pure aluminium. Fig-5: Wear verses time keeping speed constant (300 rpm) at two different loads 100 and 130 N for pure Al, duralumin and MMNC. Fig. 5 shows the wear verses time keeping speed constant at 300 rpm under 100 N and 130 N load. It is observed that wear of MMNCs increases gradually and linearly (under 100N) as time increases up to 1800 seconds. But when load increases from 100N to 130 N, wear increases to 600 µm (under 130N) from 300 µm (under 100N) suddenly and then remains nearly constant up to 1800 seconds. In both the load conditions, MMNC covers 1800 seconds. In case of duralumin, the wear is 500 µm under 100N load covering 1800 seconds and 2000 µm under 130N load covering only 300 seconds, whereas, in case of pure aluminium, the wear increases to 1400 µm under 100N load covering 900 sec and 1200 µm under 130 N load covering 600 seconds. This happens because of bonding of nano particles embedded in the aluminium matrix uniformly. Fig-6: Weight loss verses sliding distance under constant load (100 N) at two different speeds 300rpm and 350 rpm for pure Al, duralumin and MMNC. Figure 6 shows weight loss verses sliding distance keeping load constant at two different speeds. Weight loss for MMNC at 100N is nearly zero at 300 and 350 rpm though
  • 4. IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308 _______________________________________________________________________________________ Volume: 04 Issue: 04 | Apr-2015, Available @ http://www.ijret.org 596 there is a little difference which is not so significant where as in case of duralumin, wt. loss rises first within few meters of sliding distance and then becomes uniform over the whole sliding distance. When speed increases to 350 rpm, initially wt. loss rises severely and then falls and continues almost uniformly up to 900 meters of sliding distance. For duralumin, wt. loss is significantly varying under both the conditions. In case of pure aluminium, when rpm varies from 300 rpm to 350 rpm, weight loss of material varies significantly as shown. Initially the material is sticking to the wheel which indicates negative. Fig-7: Weight loss verses sliding distance keeping speed constant (300 rpm) at two different loads 100 and 130 N for pure Al, duralumin and MMNC. Figure 7 shows weight loss verses sliding distance keeping speed constant at two different loads. Weight loss for MMNC at 300 rpm is nearly zero at100N and 130N rpm though there is a little difference which is not so significant whereas in case of both duralumin and pure aluminium, when load varies from 100N to 130N, weight loss of material varies significantly as shown. Initially duralumin and pure aluminium is sticking to the wheel which indicates negative. Fig-8: Force of friction verses time keeping load (100 N) constant at two different speeds 300 and 350 rpm for MMNC, duralumin and pure aluminium. The characteristic curves between force of friction and time for pure aluminium, duralumin and MMNC specimens with constant load of 100N and at two different speeds of 300 and 350 rpm are shown in Fig 8. For MMNC in both the conditions, the force of friction is constant over the entire time period of 1800 seconds. When speed rises to 350 rpm from 300 rpm, the force of friction reduces. In case of pure aluminium, force of friction is zero under both he speeds of 300 rpm and 350 rpm. As the material is sticking to the wheel, the characteristic curves in both the cases show negative throughout 900 seconds (under 100 N) and 300 seconds (under 130 N) of time periods they covered respectively. At 300 rpm, in case of duralumin, the force of friction curve is uniform throughout the entire sliding distance of 1800 seconds with little frictional resistance whereas under 350 rpm, the alloy material is sticking to the wheel for which the characteristic curve shows negative throughout 800 seconds of time period it covered. Friction is more in case of MMNC compared to pure Al and alloy and hence, resistance to wear is more in case of MMNC. Fig-9: Force of friction verses time keeping speed constant (300 rpm) at two different loads 100 and 130 N for pure Al, duralumin and MMNC. The characteristic curves between force of friction and time for pure aluminium, duralumin and MMNC specimens with constant speed of 300 rpm and at two different loads of 100 N and 130 N are shown in Fig 9. For MMNC, at 100 N, the coeff. of friction is constant over the entire time period of 1800 seconds and at 130 N, the curve initially rises and then reduces and moves almost uniformly over the entire time period of 1800 seconds. When load rises to 130 N, the force of friction reduces. In case of duralumin, under 100 N load, the curve is uniform over the entire time period, but when load rises to 130 N, the material is sticking to the wheel and hence, the characteristic curve shows negative. It covers only 300 seconds. In case of pure aluminium, force of friction is zero under both 100 N and 130 N. As the material is sticking to the wheel, the characteristic curves show negative throughout 900 seconds (under 100 N) and 600 seconds (under 130 N) of time periods respectively. Friction is more in case of MMNC specimen compared to pure Al and alloy.
  • 5. IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308 _______________________________________________________________________________________ Volume: 04 Issue: 04 | Apr-2015, Available @ http://www.ijret.org 597 4. MICROSCOPIC EVALUATION The microstructure of the worn out samples were evaluated under FESEM. The FESEM images are shown in the figures below. Fig-10 Microstructure of pure Al at 100N and 300 rpm Fig-11 Microstructure of alloy at 100N and 300 rpm Fig-12 Microstructure of MMNC at 100N and 300 rpm Fig. 13 Microstructure of pure Al at 100N and 350 rpm
  • 6. IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308 _______________________________________________________________________________________ Volume: 04 Issue: 04 | Apr-2015, Available @ http://www.ijret.org 598 Fig. 14 Microstructure of alloy at 100N and 350 rpm Fig. 15 Microstructure of MMNC at 100N and 350 rpm Fig. 16 Microstructure of pure Al at 130N and 300 rpm Fig. 17 Microstructure of alloy at 130N and 300 rpm Fig. 18 Microstructure of MMNC at 130N and 300 rpm
  • 7. IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308 _______________________________________________________________________________________ Volume: 04 Issue: 04 | Apr-2015, Available @ http://www.ijret.org 599 Figure 10, 11 and 12 show the FESEM micrographs of worn out surfaces of pure aluminium, alloy and MMNC respectively. From the worn out surface of pure Al in figure 10, a nodular surface is observed due to heat generation and localized welding. The metal worn out becomes more because of the sticky surfaces. From the worn out microstructure of alloy shown in fig. 11, scratches are observed and the microstructure is not that smooth for which the wear is more than MMNC. From the worn out surface of MMNC in figure 12, the morphology of worn out microstructure is nearly smooth because of which wear rate is almost negligible keeping wear constant. Figure 13, 14 and 15 show the FESEM images of worn out samples at 100N load and 350 rpm of pure aluminium, alloy and composite respectively. Figure 13 shows an irregular honey comb structure because of ploughing action whereas fig. 14 shows deep scratches on the surface of alloy because of rise in speed and figure 15 has smooth microstructure showing worn out surface of MMNC uniform. But if the FESEM of fig. 12 is compared with that of fig. 15, wear in this case is found to be more. Similarly when load increases to 130 N, the FESEM shown in figure 16, 17 and 18 show the severe wear in case of pure aluminium and alloy compared to composite. This happens due to strengthening mechanism of the nano particles embedded in the matrix. Since particles are very small and when embedded in the matrix, no projections are coming out of the surfaces. Hence, no ploughing action takes place thus keeping the wear uniform in case of MMNC. The average surface roughness value of pure Al, alloy and MMNC are Ra 10.5 µm, Ra 4.2 µm and Ra 5.04 µm respectively under 100 N load and 300 rpm speed. Similarly, it is Ra 8.4 µm, Ra 5.0 µm and Ra 6.52 µm for pure Al, alloy and MMNC respectively under 100 N load and 350 rpm speed. Again, it is Ra 3.0 µm, Ra 5.2 µm and 3.8 µm for pure Al, alloy and MMNC respectively under 130 N load and 300 rpm speed. 5. CONCLUSION As this paper reports the dry sliding wear behaviour of pure aluminium, alloy and MMNC, the following conclusions can be drawn. (a) Wear decreases as the time duration increases. (b) Wear increases with the increase in load. (c) Wear increases with the increase in speed. (d) Force of friction reduces with rise in load and speed. The results shown by MMNC are encouraging in comparison to pure aluminium and duralumin as far as wear, material loss and friction are concerned. This is because of the strengthening mechanism due to uniform dispersion of Al2O3 nano particles in the matrix. Addition of nano alumina powder to aluminium increases the mechanical and tribological properties of MMNC. It also improves the hardness, yield strength, wear and abrasion resistance of the composite [24]. Again this is light in weight. FUTURE SCOPE More tests are required to study all the parameters varying the load, speed, time as well as weight percentage of reinforcements. MMNCs can be prepared by varying the weight percentage of alumina and by reinforcing alumina in the matrix of duralumin. Even hybrid MMNCs can be prepared using non-contact ultrasonic cavitation method and tribological properties can be studied. REFERENCE [1]. B. K. Prasad, K. Venkateshwaralu, O.P. Modi, S Das, A. K. Jha, R. Dasgupta, ―Effects of SiC dispersion on the sliding wear characteristics of an Al-Cu alloy‖ Proceedings of the International Conference on Aluminium, INCAL'98, New Delhi, 1998, pp.9-16. [2]. M. Saxena, O.P. Modi, B.K. Prasad, A.K. Jha, ―Erosion and corrosion characteristics of an aluminium alloy-alumina fibre composite‖ Wear 169 (1993) 119. [3]. K.K. Chawla, ―Composite Materials––Science and Engineering‖, Second edition. Springer- Verlag, New York, Pp.102, 1997. [4]. I. Sinclair, P.J. Gregson, ―Structural Performance of Discontinuous Metal Matrix Composites‖, Material Science and Technology, Vol. 3, Pp.709 – 725, 1997. [5]. I. A. Ibrahim, F.A. Mohamed, E.J. Lavernia, ―Metal Matrix Composites—A Review,‖ Journal of Material Science, Vol. 26, No. 5, 1991, pp. 1137-1157. doi:10.1007/BF00544448. [6]. Hsiao Yeh Chu, Jen Fin Lin. ―Experimental Analysis of the Tribological Behavior of Electroless Nickel-Coated Graphite Particles in Aluminum Matrix Composites under Reciprocating Motion‖, Wear Vol. 239, Pp. 126 – 142, 2000. [7]. Lim, S. C., Gupta, M., Ren, L., Kwok, J. K. M. , 1999, ―The Tribological Properties of Al-Cu/SiCp Metal Matrix Composites Fabricated using the Rheocasting Technique‖ Journal of Materials Processing Technology, Vol. (89 – 90), pp. 591 – 596. [8]. S C Lim, M Gupta, L Ren, J K M Kwok, ―The tribological properties of Al-Cu/SiC metal matrix composites fabricated using the rheocasting technique‖, Journal of material processing and Technology, 1999, 90, 591-596. [9]. Gencaga Purcek, Temel Savaskan, Samuel Murphy, ―Dry sliding friction and wear,properties of zinc based alloy‖, Wear, 2002, 252, 894 – 901. [10]. J K M Kwok, S C Lim, ―High speed tribological properties of Al/SiC composites: Frictional and wear rate characteristics‖, Composites Science and Technology, 1999, 59, 55 – 63. [11]. J K M Kwok, S C Lim, ―High speed tribological properties of Al/SiC composites: II, wear mechanisms‖, Composites Science and Technology, 1999, 59, 65 – 75. [12]. Xie Xianquing, Zhang Di, Liu Jinshui, ―Thermal expansion properties of TiC particle, reinforced ZA43 matrix composite‖, Materials and Design, 2001, 22, 157 – 162. [13]. KATO K. Wear in relation to friction- A review [J]. Wear 2000, 241(2): 151-157.
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