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International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 05 | May 2019 www.irjet.net p-ISSN: 2395-0072
© 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 6137
Effect of Reinforcement of B4C & SiC on Hardness of AA2024
Arnav1, Ankit Kumar Yadav2, Saddaf Kamran Ali3, S.M. Uruf Negami4,
Er. Rahul Malik5, Vishal Sharma6
1,2,3,4,5B.tech Student, Mechanical Engineering, P.M. College of Engineering, Sonepat, Haryana,India
2Head of Department, Mechanical Engineering, P.M. College of Engineering, Sonepat, Haryana,India
3Assistant Professor, Mechanical Engineering, P.M. College of Engineering, Sonepat, Haryana,India
---------------------------------------------------------------------***---------------------------------------------------------------------
1. ABSTRACT:- Aluminium matrix compositesareemerging
as advance engineering materials due to their strength,
ductility and toughness. The aluminium matrix can be
strengthened by reinforcing with hard ceramics particles
like silicon carbide and boron carbide etc. In the present
study, an effort is made to enhance the mechanical
properties like tensile and hardness of AMCs by reinforcing
2024 Al matrix with boron carbide and silicon carbide
particles by stir casting route.It is observed that by adding
5% reinforcement our hardness brinell hardness as well as
Rockwell hardness becomes 49 BHN and 119 HRB.And
further adding 10% reinforcement our hardness brinell as
well as Rockwell hardness is 97 BHN and 185 HRB
respectively.
2. INTRODUCTION
AA 2024 is an aluminium alloy, with copper as the primary
alloying element. It is used in application requiring high
strength to weight ratio, as well as good fatigue resistance. It
is weld able only through friction welding, and has average
machinability. Due to poor corrosion resistance, it is often
clad with aluminium. Boron carbide is an extremely hard
boron-carbon ceramic, and covalent material used in tank a
more, bullet proof vests, engine sabotagepowders,aswell as
numerous industrial applications.Witha Vickershardnessof
>30GPa, it is one of the hardest known materials, behind
cubic boron nitride and diamond.Ithas density2.52gm/cm3.
It has a melting point of 2763oC. It has a boiling point of
3500oC. Silicon carbide is used as abrasive material inwhich
molecules are bounded together by sintering to form very
hard ceramic that are widely used in applications requiring
high endurance, such as car brakes, car clutchesandceramic
plate in bullet proof vests. Electronic applications of Silicon
carbide such as light emitting diodes and detectors in early
radios were first demonstrated around1907.Siliconcarbide
is used in semiconductors electronics devices that operates
at high temperature or high voltage or both. It has density
3.16gmcm3. It has a melting point 2830oC. Upon
reinforcement of boron carbide and silicon carbide on AA
2024 its hardness as well as strength will be increasedaswe
had concluding from our research. In the present
investigations an attempt has been made on the study of
behavior of Aluminum Alloy (AA2024) reinforcing with
varying amount of B4C and SiC.Thecompositeisprepared by
stir casting process. Several fabrication techniques are
available for the production of aluminum metal matrix
composites (AMMC). Among the various methods, stir
casting route is simple, less expensive, and used for mass
production. The experimental study is performed varying
weight % of Boron Carbide and Silicon carbide powder. And
certain observations are made. The mechanical behavior of
these composites with different wt. % of mixture of Silicon
Carbide and Boron Carbide are investigated by Rockwell
Hardness Test and Brinell Hardness Test.
3. LITERATURE REVIEW
This chapter present a review of the literaturedata available
on the effect of various reinforcement types, their size and
volume fraction, ageing behavior with Al based MMC.
 J.R.S. David, D.R.S. Robinson (2013) studied the
fabrication of AMCs reinforced with various weight
percentages of SiC particulates and a constant
weight percentage of fly ash are modify by stir
casting route. The amount of wettabiility of SiC and
fly ash in the matrix was improved by adding
magnesium into the melt. The micro-structure and
mechanical properties of the fabricated AMCs were
analyzed. The SEM micrographs revealed that the
addition pf fly ash helps to prevent the dissolution
and the formation.
 J. Lakshmipathy, B. Kulendran, (2014) studied
the wear behavior of Al/SiC and Al/Al2O3
composites were prepared by stircastingtechnique
to find out the effect of weight percentage of silicon
carbide/aluminium oxide the load and the number
of stroke on a reciprocating wear testing machine.
The tests are carried out with different load
conditions (25, 50 and 75 N) and different number
of stroke (420, 780 and 1605 strokes).
 L. Yuan, J. Han, J. Liu, Z. Jiang (2016) studied
about aluminium composite matrix reinforced with
AlB2 particles have been fabricated using a
combination of powder metallurgy and heat
treatment solution. The heat treatment parameters
on the microstructure and mechanical propertiesof
the composites were investigated by means of SEM
and micro hardness test. The friction coefficient,
wear behavior and scratch morphologyoftheAMCs
and pure aluminium werealsostudiedusingscratch
tests.
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 05 | May 2019 www.irjet.net p-ISSN: 2395-0072
© 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 6138
 R. Harichandran, N. Selvakumar (2016) studied
the fabricated micro and nano Boron carbide
particles-reinforced compositeswerecharacterized
using SEM and X-ray method. Tensile, hardness
impact and wear tests were carried out in order to
evaluate the mechanical propertiesofthemicroand
nano composites. The tensile test results showed
that the properties of the samples containingupto6
%. Nano Boron carbide reinforced compositeswere
better that the micro Boron carbide reinforced
composites.
 Y. Sahin (2016) studied the Aluminium alloy
composites containing various particles size of 10
and 20 wt. % SiC particles. It was observed that
there was a reasonably uniform dispersion of
particles in the matrix alloy. The density decreased
with decreasing particles size but porosity
decreased considerably with changing particlesize.
In addition the tool life gets decreased considerably
with increasing cutting speed for all sets.
 K. Ravikumar, K. Kiran, V.S. Sreebalaji (2017)
studied the investigation on mechanical properties
of Aluminuim alloy (AA 6082) composites
reinforced with tungsten carbide particles. Stir
casting process was employed to fabricate the
aluminum composite specimen by changing
tungsten carbide in 2, 4, 6, 8 and 10 % by weight.
The result is that density and impact strength and
the elongation of the composite decreased with
increased in tungsten carbide. The tensile strength
of the composite changes initially and then tends to
decrease
 K.K. Alaneme, O.B. Michael, A.A. Adebimpe
(2018) studied the mechanical properties of
aluminium composites reinforced with ground nut
shell (GSA) and SiC was investigated. Ground nut
shell and Silicon carbide with various mixing ratio
(10:0, 7.5:2.5, 5.0: 5.0, 2.5: 7.5 and 0.10) constituted
6 and 10 wt. % of the reinforcing phase while the
matrix matrial was Al-Mg-Si alloy. The result shows
that with increasing of Ground nut shell in the
reinforcing phase the gardness and ultimate
strength of tensile and specific strength of the
composites owing to the amount of the oxides of Al,
Si, Ca, K2 and Mg were presenting the composition
of GSA.
4. RESEARCH GAPS
 Although a large volume of literature is available on
composite materials, the topic is still under
development and offers potential opportunity for
further research and application.
 Many researchers have conducted the machining
study on aluminum based metal matrixcomposites
with SiC, boron carbide, alumina, zirconia, etc., as
the reinforcements. But,very fewhaveinvestigated
on hybrid composite.
 Few studies have been reported on composite such
as AA-SiC and AA-B4C composite. However, no
studies have been carried out in Al-SiC-B4C
composite.
 Less research works have been reported on
aluminium based (Al2024) MMCs which offer
better machinability and surfacefinishcapabilities,
than pure aluminium matrix, so there is plenty of
scope to explore the manufacturing of MMCs.
5. OBJECTIVE
The main purpose of this project is to develop the strong
light weighted metal matrix Al-SiC+B4C composite material
which is useful in the industrial sectors as well as advanced
machineries. The most important part of this project is to
fabricate Al-SiC+B4C metal-matrix of by homogeneous stir-
casting to produce High Strength Low Cost Material
(HSLCM). We adopt the stir-casting method with high
temperature in this project. This types of metal-matrix
composite have very high specific strength, temperature
resistance, fatigue resistance, abrasion resistance,corrosion
resistance and stiffness properties that they are used in
Aircraft fittings, gearsandshafts,bolts,clock parts,computer
parts, couplings, fuse parts, hydraulic valve bodies, missile
parts, munitions, nuts, pistons, rectifier parts, worm gears,
fastening devices, veterinary and orthopedic equipment,
structures. The objective of the project are:
 Development of Al-SiC+B4C composite by varying
the reinforcement percentage from 0 to 10% in a
step of 5 %.
 To measure the Micro hardness (HRB)ofdeveloped
composite and its comparison with base metal.
 To measure the Macro hardness (BHN) of
developed composite and its comparisonwith base
metal.
6. EXPERIMENTAL PROCEDURE
A lot of 1000 g of aluminium alloy (AA2024) was measured
and put in the crucible and was melted at 7240C using an
electric furnace. Proper stirring is required in order to
achieve uniform spreading of reinforcement in the
aluminium melt. The melt was stirred with the help of a
mechanical stirrer to form a fine vortex. To oxidize the
surface of ceramic particulates, theSiC+B4C ceramicpowder
was preheated with the help of reinforcement preheat set-
up. This preheated ceramic powder was supplied at a
constant feed rate into vortex of aluminium melt.
Argon gas was provided into the melt duringprocesstooffer
an inert troposphere. Afterstirringthemoltenmixtureit was
poured in to a preheated permanent mold. Argon gas was
supplied until the entire melt was poured intothepreheated
permanent mold. The manufactured hybrid composite was
allowed to solidify in atmospheric air and was taken out
from the mold after solidification.TheAMCshavingdifferent
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 05 | May 2019 www.irjet.net p-ISSN: 2395-0072
© 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 6139
weight percentage (5 and 10) SiC+B4C (5% means equal
amount of both reinforcements i.e. 2.5% each, similarly 5%
each in case of 10%) ceramic powder were manufactured by
the same procedure.
 Mechanical stirring is necessary to help in
promoting wettability.
 Stirring in a fully liquid condition does not help to
incorporate particles into the matrix.
 Stirring while the slurry (melt of matrix and
reinforcement) is solidifying improves
incorporation of the particles into the matrix alloy
.However the slurry must then be re-melted to a
fully liquid condition in order to enable pouring
into a mold .A decrease in solidifying time during
stirring increases the percentage wetting. The
particles tend to float to the top of the molten alloy,
regardless of the speed of stirring. The processing
temperature is mainly influencing the change in
viscosity of Al matrix and it also accelerates the
chemical reaction b/w matrix and reinforcement.
The change of viscosity influences the particle
distribution in the matrix. The viscosity of liquid
decreasedwhenincreasingprocessingtemperature
with increasing holding time (stirring time).Effect
of holding time helps in hybrid composite mainly
two ways: to distribute the particles in the liquid
and to create perfect interface bond b/w
reinforcement and matrix. The holding time b/w
matrix and reinforcement is considered as
important factor in the processing of composite.
When the holding time is less the particles are
distributed uniformly in the matrix the liquid
matrix has sufficient viscosity in the temperature
range and velocity of particle flow is small. In case
of large holding time the liquid has sufficient
viscosity at lower temperature butthecontacttime
b/w the matrix and reinforcement too large during
this period the particles are distributed uniformly
in the liquid even though some of particles form
clusters which could be also located in the matrix
region. a vortex createdduringstirringcansuck the
air bubbles or gas bubbles in to the liquid metal .as
the result the particles were attached with air
bubbles to form the particles clusters in thematrix.
At higher temperature with more holding time
more particles cluster are found in the composite
bar. Stirring time is 10 min.
7. RESULT
The mechanical properties of matrix alloy 2024 is improved
upon incorporation of mixture of Silicon Carbide and Boron
Carbide. Figure shows the relation between weight
percentages of SiC + B4C ceramic particulates and micro-
hardness of manufactured AMMCs. While next figure shows
the relation between weight percentages of SiC + B4C
ceramic particulates and macro-hardness of manufactured
AMMCs.
The mechanical properties of matrix alloy 2024 are
improved upon SiC+B4C incorporation. Figure shows the
relation between weight percentages of SiC+B4C ceramic
particulates and micro-hardness of manufactured AMCs
while Figure shows therelationbetween weightpercentages
of SiC+B4C ceramic particulates and macro-hardness of
manufactured AMCs. It is revealed that micro and macro-
hardness of AMCs are increasing linearly with increase in
weight percentage of SiC+B4C ceramicparticulates.This may
be attributed because of increase in presence of hard
ceramics particles in the alloy and high hardness of
reinforcement. Incorporation of reinforcement particles in
the aluminium metal matrix increase their surface area and
the size of aluminium metal matrix grains are reduced. The
presence of these hard surface area of SiC+B4C ceramic
particulates offer large resistance to the plastic deformation
which results into enhancement of the hardness of
manufactured AMCs. Further, the presence of hard and
brittle SiC+B4C ceramic particulates in the soft and ductile
AA2024 metal matrix reduces the ductility content of
manufactured AMCs due to low ductile content of metal
matrix in the composite which significantly enhances the
hardness value of manufactured AMCs. Increasedcontent of
reinforcement in the matrix alloy leads to increased
dislocation density during solidification due to thermal
mismatch of the matrix alloy and reinforcement. The
mismatch of thermal expansion between matrix and
reinforcement due to temperature difference resultsinlarge
internal stress due to which matrix deforms plastically to
accommodate the smaller volume expansion of
reinforcement particles. Enhancementindislocationdensity
at the particle metal interface results in higher resistance to
plastic deformation leading to improved hardness.
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 05 | May 2019 www.irjet.net p-ISSN: 2395-0072
© 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 6140
8. FUTURE SCOPE
Due to cheaper cost and high hardness the reinforced AA
2024 has a bright future for aerospace as well as in
automobile industries because it’s corrosive and withstand
to high temperature property is also very good.
9. REFRENCES
 J.R.S. David, D.R.S. Robinson (2013) studied the
fabrication of AMCs reinforced with various weight
percentages of SiC particulates and a constant
weight percentage of fly ash are modify by stir
casting route.
 L. Yuan, J. Han, J. Liu, Z. Jiang (2016) studied
about aluminium composite matrix reinforced with
AlB2 particles have been fabricated using a
combination of powder metallurgy and heat
treatment solution R. Harichandran, N.
Selvakumar (2016) studied the fabricated micro
and nano Boron carbide particles-reinforced
composites werecharacterizedusingSEMandX-ray
method.
 K. Ravikumar, K. Kiran, V.S. Sreebalaji (2017)
studied the investigation on mechanical properties
of Aluminuim alloy (AA 6082) composites
reinforced with tungsten carbide particles
 K.K. Alaneme, O.B. Michael, A.A. Adebimpe
(2018) studied the mechanical properties of
aluminium composites reinforced with ground nut
shell (GSA) and SiC was investigated.

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IRJET- Effect of Reinforcement of B4C & SIC on Hardness of AA2024

  • 1. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 05 | May 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 6137 Effect of Reinforcement of B4C & SiC on Hardness of AA2024 Arnav1, Ankit Kumar Yadav2, Saddaf Kamran Ali3, S.M. Uruf Negami4, Er. Rahul Malik5, Vishal Sharma6 1,2,3,4,5B.tech Student, Mechanical Engineering, P.M. College of Engineering, Sonepat, Haryana,India 2Head of Department, Mechanical Engineering, P.M. College of Engineering, Sonepat, Haryana,India 3Assistant Professor, Mechanical Engineering, P.M. College of Engineering, Sonepat, Haryana,India ---------------------------------------------------------------------***--------------------------------------------------------------------- 1. ABSTRACT:- Aluminium matrix compositesareemerging as advance engineering materials due to their strength, ductility and toughness. The aluminium matrix can be strengthened by reinforcing with hard ceramics particles like silicon carbide and boron carbide etc. In the present study, an effort is made to enhance the mechanical properties like tensile and hardness of AMCs by reinforcing 2024 Al matrix with boron carbide and silicon carbide particles by stir casting route.It is observed that by adding 5% reinforcement our hardness brinell hardness as well as Rockwell hardness becomes 49 BHN and 119 HRB.And further adding 10% reinforcement our hardness brinell as well as Rockwell hardness is 97 BHN and 185 HRB respectively. 2. INTRODUCTION AA 2024 is an aluminium alloy, with copper as the primary alloying element. It is used in application requiring high strength to weight ratio, as well as good fatigue resistance. It is weld able only through friction welding, and has average machinability. Due to poor corrosion resistance, it is often clad with aluminium. Boron carbide is an extremely hard boron-carbon ceramic, and covalent material used in tank a more, bullet proof vests, engine sabotagepowders,aswell as numerous industrial applications.Witha Vickershardnessof >30GPa, it is one of the hardest known materials, behind cubic boron nitride and diamond.Ithas density2.52gm/cm3. It has a melting point of 2763oC. It has a boiling point of 3500oC. Silicon carbide is used as abrasive material inwhich molecules are bounded together by sintering to form very hard ceramic that are widely used in applications requiring high endurance, such as car brakes, car clutchesandceramic plate in bullet proof vests. Electronic applications of Silicon carbide such as light emitting diodes and detectors in early radios were first demonstrated around1907.Siliconcarbide is used in semiconductors electronics devices that operates at high temperature or high voltage or both. It has density 3.16gmcm3. It has a melting point 2830oC. Upon reinforcement of boron carbide and silicon carbide on AA 2024 its hardness as well as strength will be increasedaswe had concluding from our research. In the present investigations an attempt has been made on the study of behavior of Aluminum Alloy (AA2024) reinforcing with varying amount of B4C and SiC.Thecompositeisprepared by stir casting process. Several fabrication techniques are available for the production of aluminum metal matrix composites (AMMC). Among the various methods, stir casting route is simple, less expensive, and used for mass production. The experimental study is performed varying weight % of Boron Carbide and Silicon carbide powder. And certain observations are made. The mechanical behavior of these composites with different wt. % of mixture of Silicon Carbide and Boron Carbide are investigated by Rockwell Hardness Test and Brinell Hardness Test. 3. LITERATURE REVIEW This chapter present a review of the literaturedata available on the effect of various reinforcement types, their size and volume fraction, ageing behavior with Al based MMC.  J.R.S. David, D.R.S. Robinson (2013) studied the fabrication of AMCs reinforced with various weight percentages of SiC particulates and a constant weight percentage of fly ash are modify by stir casting route. The amount of wettabiility of SiC and fly ash in the matrix was improved by adding magnesium into the melt. The micro-structure and mechanical properties of the fabricated AMCs were analyzed. The SEM micrographs revealed that the addition pf fly ash helps to prevent the dissolution and the formation.  J. Lakshmipathy, B. Kulendran, (2014) studied the wear behavior of Al/SiC and Al/Al2O3 composites were prepared by stircastingtechnique to find out the effect of weight percentage of silicon carbide/aluminium oxide the load and the number of stroke on a reciprocating wear testing machine. The tests are carried out with different load conditions (25, 50 and 75 N) and different number of stroke (420, 780 and 1605 strokes).  L. Yuan, J. Han, J. Liu, Z. Jiang (2016) studied about aluminium composite matrix reinforced with AlB2 particles have been fabricated using a combination of powder metallurgy and heat treatment solution. The heat treatment parameters on the microstructure and mechanical propertiesof the composites were investigated by means of SEM and micro hardness test. The friction coefficient, wear behavior and scratch morphologyoftheAMCs and pure aluminium werealsostudiedusingscratch tests.
  • 2. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 05 | May 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 6138  R. Harichandran, N. Selvakumar (2016) studied the fabricated micro and nano Boron carbide particles-reinforced compositeswerecharacterized using SEM and X-ray method. Tensile, hardness impact and wear tests were carried out in order to evaluate the mechanical propertiesofthemicroand nano composites. The tensile test results showed that the properties of the samples containingupto6 %. Nano Boron carbide reinforced compositeswere better that the micro Boron carbide reinforced composites.  Y. Sahin (2016) studied the Aluminium alloy composites containing various particles size of 10 and 20 wt. % SiC particles. It was observed that there was a reasonably uniform dispersion of particles in the matrix alloy. The density decreased with decreasing particles size but porosity decreased considerably with changing particlesize. In addition the tool life gets decreased considerably with increasing cutting speed for all sets.  K. Ravikumar, K. Kiran, V.S. Sreebalaji (2017) studied the investigation on mechanical properties of Aluminuim alloy (AA 6082) composites reinforced with tungsten carbide particles. Stir casting process was employed to fabricate the aluminum composite specimen by changing tungsten carbide in 2, 4, 6, 8 and 10 % by weight. The result is that density and impact strength and the elongation of the composite decreased with increased in tungsten carbide. The tensile strength of the composite changes initially and then tends to decrease  K.K. Alaneme, O.B. Michael, A.A. Adebimpe (2018) studied the mechanical properties of aluminium composites reinforced with ground nut shell (GSA) and SiC was investigated. Ground nut shell and Silicon carbide with various mixing ratio (10:0, 7.5:2.5, 5.0: 5.0, 2.5: 7.5 and 0.10) constituted 6 and 10 wt. % of the reinforcing phase while the matrix matrial was Al-Mg-Si alloy. The result shows that with increasing of Ground nut shell in the reinforcing phase the gardness and ultimate strength of tensile and specific strength of the composites owing to the amount of the oxides of Al, Si, Ca, K2 and Mg were presenting the composition of GSA. 4. RESEARCH GAPS  Although a large volume of literature is available on composite materials, the topic is still under development and offers potential opportunity for further research and application.  Many researchers have conducted the machining study on aluminum based metal matrixcomposites with SiC, boron carbide, alumina, zirconia, etc., as the reinforcements. But,very fewhaveinvestigated on hybrid composite.  Few studies have been reported on composite such as AA-SiC and AA-B4C composite. However, no studies have been carried out in Al-SiC-B4C composite.  Less research works have been reported on aluminium based (Al2024) MMCs which offer better machinability and surfacefinishcapabilities, than pure aluminium matrix, so there is plenty of scope to explore the manufacturing of MMCs. 5. OBJECTIVE The main purpose of this project is to develop the strong light weighted metal matrix Al-SiC+B4C composite material which is useful in the industrial sectors as well as advanced machineries. The most important part of this project is to fabricate Al-SiC+B4C metal-matrix of by homogeneous stir- casting to produce High Strength Low Cost Material (HSLCM). We adopt the stir-casting method with high temperature in this project. This types of metal-matrix composite have very high specific strength, temperature resistance, fatigue resistance, abrasion resistance,corrosion resistance and stiffness properties that they are used in Aircraft fittings, gearsandshafts,bolts,clock parts,computer parts, couplings, fuse parts, hydraulic valve bodies, missile parts, munitions, nuts, pistons, rectifier parts, worm gears, fastening devices, veterinary and orthopedic equipment, structures. The objective of the project are:  Development of Al-SiC+B4C composite by varying the reinforcement percentage from 0 to 10% in a step of 5 %.  To measure the Micro hardness (HRB)ofdeveloped composite and its comparison with base metal.  To measure the Macro hardness (BHN) of developed composite and its comparisonwith base metal. 6. EXPERIMENTAL PROCEDURE A lot of 1000 g of aluminium alloy (AA2024) was measured and put in the crucible and was melted at 7240C using an electric furnace. Proper stirring is required in order to achieve uniform spreading of reinforcement in the aluminium melt. The melt was stirred with the help of a mechanical stirrer to form a fine vortex. To oxidize the surface of ceramic particulates, theSiC+B4C ceramicpowder was preheated with the help of reinforcement preheat set- up. This preheated ceramic powder was supplied at a constant feed rate into vortex of aluminium melt. Argon gas was provided into the melt duringprocesstooffer an inert troposphere. Afterstirringthemoltenmixtureit was poured in to a preheated permanent mold. Argon gas was supplied until the entire melt was poured intothepreheated permanent mold. The manufactured hybrid composite was allowed to solidify in atmospheric air and was taken out from the mold after solidification.TheAMCshavingdifferent
  • 3. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 05 | May 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 6139 weight percentage (5 and 10) SiC+B4C (5% means equal amount of both reinforcements i.e. 2.5% each, similarly 5% each in case of 10%) ceramic powder were manufactured by the same procedure.  Mechanical stirring is necessary to help in promoting wettability.  Stirring in a fully liquid condition does not help to incorporate particles into the matrix.  Stirring while the slurry (melt of matrix and reinforcement) is solidifying improves incorporation of the particles into the matrix alloy .However the slurry must then be re-melted to a fully liquid condition in order to enable pouring into a mold .A decrease in solidifying time during stirring increases the percentage wetting. The particles tend to float to the top of the molten alloy, regardless of the speed of stirring. The processing temperature is mainly influencing the change in viscosity of Al matrix and it also accelerates the chemical reaction b/w matrix and reinforcement. The change of viscosity influences the particle distribution in the matrix. The viscosity of liquid decreasedwhenincreasingprocessingtemperature with increasing holding time (stirring time).Effect of holding time helps in hybrid composite mainly two ways: to distribute the particles in the liquid and to create perfect interface bond b/w reinforcement and matrix. The holding time b/w matrix and reinforcement is considered as important factor in the processing of composite. When the holding time is less the particles are distributed uniformly in the matrix the liquid matrix has sufficient viscosity in the temperature range and velocity of particle flow is small. In case of large holding time the liquid has sufficient viscosity at lower temperature butthecontacttime b/w the matrix and reinforcement too large during this period the particles are distributed uniformly in the liquid even though some of particles form clusters which could be also located in the matrix region. a vortex createdduringstirringcansuck the air bubbles or gas bubbles in to the liquid metal .as the result the particles were attached with air bubbles to form the particles clusters in thematrix. At higher temperature with more holding time more particles cluster are found in the composite bar. Stirring time is 10 min. 7. RESULT The mechanical properties of matrix alloy 2024 is improved upon incorporation of mixture of Silicon Carbide and Boron Carbide. Figure shows the relation between weight percentages of SiC + B4C ceramic particulates and micro- hardness of manufactured AMMCs. While next figure shows the relation between weight percentages of SiC + B4C ceramic particulates and macro-hardness of manufactured AMMCs. The mechanical properties of matrix alloy 2024 are improved upon SiC+B4C incorporation. Figure shows the relation between weight percentages of SiC+B4C ceramic particulates and micro-hardness of manufactured AMCs while Figure shows therelationbetween weightpercentages of SiC+B4C ceramic particulates and macro-hardness of manufactured AMCs. It is revealed that micro and macro- hardness of AMCs are increasing linearly with increase in weight percentage of SiC+B4C ceramicparticulates.This may be attributed because of increase in presence of hard ceramics particles in the alloy and high hardness of reinforcement. Incorporation of reinforcement particles in the aluminium metal matrix increase their surface area and the size of aluminium metal matrix grains are reduced. The presence of these hard surface area of SiC+B4C ceramic particulates offer large resistance to the plastic deformation which results into enhancement of the hardness of manufactured AMCs. Further, the presence of hard and brittle SiC+B4C ceramic particulates in the soft and ductile AA2024 metal matrix reduces the ductility content of manufactured AMCs due to low ductile content of metal matrix in the composite which significantly enhances the hardness value of manufactured AMCs. Increasedcontent of reinforcement in the matrix alloy leads to increased dislocation density during solidification due to thermal mismatch of the matrix alloy and reinforcement. The mismatch of thermal expansion between matrix and reinforcement due to temperature difference resultsinlarge internal stress due to which matrix deforms plastically to accommodate the smaller volume expansion of reinforcement particles. Enhancementindislocationdensity at the particle metal interface results in higher resistance to plastic deformation leading to improved hardness.
  • 4. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 05 | May 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 6140 8. FUTURE SCOPE Due to cheaper cost and high hardness the reinforced AA 2024 has a bright future for aerospace as well as in automobile industries because it’s corrosive and withstand to high temperature property is also very good. 9. REFRENCES  J.R.S. David, D.R.S. Robinson (2013) studied the fabrication of AMCs reinforced with various weight percentages of SiC particulates and a constant weight percentage of fly ash are modify by stir casting route.  L. Yuan, J. Han, J. Liu, Z. Jiang (2016) studied about aluminium composite matrix reinforced with AlB2 particles have been fabricated using a combination of powder metallurgy and heat treatment solution R. Harichandran, N. Selvakumar (2016) studied the fabricated micro and nano Boron carbide particles-reinforced composites werecharacterizedusingSEMandX-ray method.  K. Ravikumar, K. Kiran, V.S. Sreebalaji (2017) studied the investigation on mechanical properties of Aluminuim alloy (AA 6082) composites reinforced with tungsten carbide particles  K.K. Alaneme, O.B. Michael, A.A. Adebimpe (2018) studied the mechanical properties of aluminium composites reinforced with ground nut shell (GSA) and SiC was investigated.