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7/31/2019 The Effect of Compression Load, Sintering Temperature and Sintering Time During Production the of Aluminum Based Metal Matrix Composites
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The Effect of Compression Load, Sintering Temperature and Sintering Time
during Production the of Aluminum Based Metal Matrix Composites
Raghunath.K1, Rajkumar.D
2, Pon swarna raja pandian.S
3, Rajesh.S
4
1, 2, 3: Final Year Mechanical Engineering, Kalasalingam University, Krishnankoil.
4: Assistant Professor, Mechanical Engineering, Kalasalingam University, Krishnankoil.
Contact No 1, 2,3: 9486123764,9486225660, 9566780890.
Email:[email protected],[email protected]
2
Abstract
In this paper attempt has been taken to fabricate aluminum based Metal Matrix Composites
(MMC) using tungsten carbide as reinforcement material and aluminum as matrix material.
During the fabrication the effect of load, sintering temperature and sintering time were analyzed.
The result reveled that increases in load, temperature and time increase the mechanical
properties of the material to the certain level. Increases in reinforcement content beyond 15%
decreases the mechanical properties of materials.
Keywords: Metal matrix composite, Aluminium, Tungsten carbide, Load, sintering
temperature and time.
Introduction
Metal matrix composites offer a number of
advantages compared to their base metals,
such as higher specific strengths and moduli,
higher elevated temperature resistance,
lower coefficients of thermal expansion,
and, in some cases, better wear resistance.
On the down side, they are more expensive
than their base metals and have lower
toughness. Metal matrix composites also
have some advantages compared to polymer
matrix composites, including higher matrix
dependent strength and moduli, higher
elevated temperature resistance, no moisture
absorption, higher electrical and thermal
conductivities, and non- flammability.
However, metal matrix composites (MMCs)
are normally more expensive than even
polymer matrix composites, and the
fabrication processes are much more limited,
especially for complex structural shapes.
Due to their high cost, commercial
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than starting with elemental blends. In
Metal matrix composite, the method of the
introduction of particles into the matrix melt
is one of the most important aspects in
composition. The commercially different
sizes of reinforcement materials are
available. In this work the average particle
of the reinforcement material is 13 to 20
microns. The aluminum powder average
particle size is 300 microns. The materials
are blended uniformly and pressed at
different loads to fabricate specimen. The
size of the specimen is 30 mm and height
may vary from 4 to 30mm. Three different
loads were applied to produce specimen,
namely 200, 250 and 300 kN. The
temperature in the furnace is varied from
500,550 and 6000C. The time in the furnace
is varied from 30 to 60 min. Three different
percentages of reinforcements were used for
fabrication and it is listed in the table 1.
Table 1
Composition Load 200KN Load 250KN Load 300KN
Weight (gm) Weight (gm) Weight (gm)
95% AL 5% WL 7 10 7 10 7 10
90% AL 10% WL 7 10 7 10 7 10
85% AL 15% WL 7 10 7 10 7 10
80%AL 20%WL 7 10 7 10 7 10
SAMPLE PREPARATION:
All samples must also be of an appropriate
size to fit in the specimen chamber and are
generally and are generally mounted rigidly
on a specimen stub. Several models of SEM
can examine any part of a 6-inch (15 cm)
semiconductor wafer, and some can tilt anobject of that size to 450. The fig I show the
sample specimen of the 5% reinforcement
composites.
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Fig 1: 5% reinforcement composites
Result and Discussion
The hardness was conducted on the
specimen and it was found that the increases
in reinforcement will increases the hardness
of the material. The table 1 shows the
Rockwell hardness value for the different
specimen.
Rockwell hardness is conducted on
composite pellets. Composition of greater
percentage (i.e. 15% composition) shows the
better result. Therefore 15% composition
can be selected for fabrication of any
automobile component.
Table 1: Hardness
Pellets Hardness(c scale)
5% 47
10% 51
15% 53
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