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International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 07 | July 2019 www.irjet.net p-ISSN: 2395-0072
© 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 1751
Tensile Property and Hardness of Al-7075 Matrix Reinforced with
Silicon Carbide Particles
Muhammed Muddassir1, S.B Mallur2
1Department of Mechanical Engineering, University B.D.T College of Engineering, Davanagere
2Professor and Chairman, University B.D.T College of Engineering, Davanagere
---------------------------------------------------------------------***----------------------------------------------------------------------
Abstract - Aluminium 7075 alloy as a matrix material
and the silicon carbide as a reinforcement material have
been used because it has potential applications in
aerospace and aircraft industries because of its low weight
to high strength ratio. It also used because it has high
wear resistance and creep resistance property. The
investigation about the tensile property and hardness of Al
7075 and silicon carbide is needed so that metal matrix
composite fabricated for the aerospace and aircraft
industries should be defect free. In this work Al 7075 is
reinforced with 0, 5, 10, 15, 20 wt % of silicon carbide by
stir casting method. The resulted casted specimens are
tested to know the tensile property and hardness of the
composite.
Key words: Al 7075, Stir casting, Tensile Strength,
Hardness.
1. INTRODUCTION
The use of metal matrix composite as structural
engineering material has more attention in current
years. Because of their more strength to low weight
ratio, and toughness at high temperature which makes
them suitable for various applications. Whereas
engineering materials like steel are used as MMC
because of its superior stiffness and high mechanical
strength compare to matrix alloys, but the major
disadvantage is its poorer ductility and lesser fracture
toughness. MMC have high tensile and compressive
stresses by transfer and distributing the applied load
from ductile matrix to the reinforcement material. The
transfer of load takes place from matrix to reinforcement
if it has interfacial bonds. Therefore appropriate
selection of matrix material and reinforcement material
with their properties and the method of fabrication
selected which effect this bond will significantly
influence the resulting MMC.
2. METHODOLOGY
The current research is carrying out on Aluminium 7075
alloy which is reinforced with silicon carbide particles.
For Al 7075 metal various weight percentage of silicon
carbide is added by stir casting technique. Five samples
each prepared for tensile test and Hardness test.
Samples are prepared by varying the silicon carbide
weight percentage as 0%, 5%, 10%, 15% and 20%. In
this process initially silicon carbide powder is preheated
at a temperature of 4000c for an hour in the muffle
furnace. After this preheated silicon carbide powder is
poured in to the molten aluminium at a temperature of
7500c.Degasifier and cover flux is added.
Hexachloroethane (c2cl6) is used as a degasifier to
remove the entrapped air and cover flux (45 % Nacl,
45% Kcl, and 10% NaF) is added to prevent oxidation
losses of aluminium during melting this improves the
yield of molten metal from the charge. The silicon
carbide powder is mixed in the molten aluminium with
the help of stirrer so that uniform supply of silicon
carbide particles in molten aluminium can be achieved.
Following stirring hold molten metal for 5minutes and
then it is poured in to the suitable moulds. The moulds in
which the molten metal is poured should be preheated in
order to keep away from thermoelectric voltage arise
due to huge differences in temperature, and not to
decrease the repair life of the moulds or scratch the
coating applied. After pouring allow the molten metal to
solidify and then take out from the mould.
Fig: 1: Muffle furnace
Fig: 2: Pouring of Molten metal
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 07 | July 2019 www.irjet.net p-ISSN: 2395-0072
© 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 1752
Fig: 3: Casted Specimens
Fig: 4: Machined Specimens
3. EXPERIMENTATION
Material Selection:
Matrix Material:
Al7075 is chosen as matrix material due to wide
applications in many engineering sectors. Aluminium
7075 is an aluminium alloy with zinc as main alloying
element. The Composition of Al7075 is shown in the
Table.
Table: 1: Composition of Al-7075
Material Zinc Mg Copper Titanium
Wt % 5.6-6.1 2.1-2.5 1.2-1.6 <0.5
Reinforcement Materials
Silicon carbide used as reinforcement material. The
properties of silicon carbide are shown in the table
below
Table 2: Properties of Sic
Mechanical Properties Values
Melting Point 0C 1400
Flexural Strength Mpa 550
Hardness 2800
Density g/cm3 3.1
Fracture Toughness Mpa/m2 4.6
Poisson’s Ratio 0.14
Composition used for Metal Matrix Composite:-
Table 3: Composition
Sample Wt. of Al-
7075
Wt. of Sic
Al-7075 with 0% Sic 240 g 0 g
Al-7075 with 5% Sic 261 g 13.05 g
Al-7075 with 10% Sic 234 g 23.4 g
Al-7075 with 15% Sic 225 g 33.75 g
Al-7075 with 20% Sic 235 g 47 g
4. Results and Discussions
4.1 Tensile Test:
The tensile test specimen is ready with size according to
ASTM standard E8. The specimen for tensile test is
shown in figure 5. The tensile test is carry out in
computerized tensometer.
Fig: 5: Specimen on Tensometer
Fig: 6: Tested Specimens
Table: 4: Ultimate Tensile Strength (Mpa)
Materials Ultimate Tensile Strength
(Mpa)
Al-7075 with 0% Sic 153.95
Al-7075 with 5% Sic 162.09
Al-7075 with 10% Sic 170.38
Al-7075 with 15% Sic 207.29
Al-7075 with 20% Sic 190.7
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 07 | July 2019 www.irjet.net p-ISSN: 2395-0072
© 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 1753
Variation in Tensile Strength:
Fig: 7: Comparison of Ultimate Tensile strength
Fig: 8: Variation of Ultimate Tensile Strength
Tensile test are perform on a Tensometer for 0, 5, 10, 15
and 20 wt% of SiC composite and the reading are
tabulate. It was practical that tensile strength increase
with the increases in wt% of SiC until 15 wt% after that
it gradually decreases as shown in the above graph.
From the above graphs it clears that for 15 wt% of SiC in
Al-7075 has maximum ultimate tensile strength.
Table: 5: % of Reduction in Area
Materials Reduction Area %
Al-7075 with 0% Sic 0.052
Al-7075 with 5% Sic 0.054
Al-7075 with 10% Sic 0.056
Al-7075 with 15% Sic 0.069
Al-7075 with 20% Sic 0.067
Fig: 9: % of Reduction in Area
From the above table it’s clear that as the percentage of
reinforcement i.e. Silicon Carbide, increase the reduction
area percentage also increase until 15 wt% of Silicon
Carbide then after this the percentage of reduction area
decreases.
4.1 Hardness Test:
The conflict of materials against surface indentation is
termed as hardness. The micro hardness of composites
evaluates the border bond strength among reinforcing
particles and matrix.
Experiment has been conduct by changeable weight
fraction of SiC (0%, 5%, 10%, 15%, and 20%). Hardness
is record and tabulate. Hardness test have been conduct
on each sample by means of a load of 30 kgf and
Pyramidal Diamond indenter whose faces are set at a
136 degree angle from one another. Dimension of
impression prepared by indenter have been predict by
microscope. The equivalent value of hardness (HV) was
calculated from standard formula.
Table: 6: Vickers Hardness Number (VHN)
Materials Vickers Hardness
Al-7075 with 0% Sic 274
Al-7075 with 5% Sic 347.62
Al-7075 with 10% Sic 365.68
Al-7075 with 15% Sic 385.18
Al-7075 with 20% Sic 375.24
Fig: 10: Comparison of VHN
0
50
100
150
200
250
Al 7075 +
0% Sic
Al 7075 +
5% Sic
Al 7075 +
10% Sic
Al 7075 +
15% Sic
Al 7075 +
20% Sic
Ultimate Tensile Strength (Mpa)
153.95 162.09
170.38
207.29
190.7
0
50
100
150
200
250
Al 7075
+ 0%
Sic
Al 7075
+ 5%
Sic
Al 7075
+ 10%
Sic
Al 7075
+ 15%
Sic
Al 7075
+ 20%
Sic
Ultimate Tensile Strength (Mpa)
2.069
1.7507
1.4324
1.114 1.2732
Al 7075 +
0% Sic
Al 7075 +
5% Sic
Al 7075 +
10% Sic
Al 7075 +
15% Sic
Al 7075 +
20% Sic
Reducton Area %
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 07 | July 2019 www.irjet.net p-ISSN: 2395-0072
© 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 1754
Above table show the Vickers hardness numbers of
composite contain varying wt. % of SiC reinforcements.
The chart shows that adding of SiC particles in Al7075
matrix composites enhance the hardness composite,
when compare with unreinforced Al7075. When
unreinforced Al7075 have Vickers hardness number
(274), hardness rate increase with increase in SiC
content and utmost hardness value obtained is (385.18)
for 15 wt. % SiC reinforced Al7075 matrix. The
existences of harder and well bonded SiC particles in
Al7075 matrix that obstruct the movement of dislocation
increase the hardness of composite.
5. CONCLUSIONS:
In this experimental study, Aluminium 7075 is
reinforced with varying silicon carbide content (0, 5, 10,
15, 20 wt %) be prepared by using stir casting
manufacture method. Tensile strength and hardness of
the ready samples is calculated.
Base on the investigational results the following
conclusion is made:-
The adding of silicon carbide in the Aluminium 7075
matrix increases the tensile strength and Vickers
hardness when compared with unreinforced Aluminium
7075.
15 wt % of silicon carbide content in Aluminium 7075
matrix composite the maximum tensile strength and
hardness.
From the outcome above, silicon carbide reinforced
Aluminium 7075 matrix composite showed better tensile
strength and hardness than the unreinforced Aluminium
7075.
References:
1. Md. Habibur Rahman, H. M. Mamun Al Rashed.
"Characterization of Silicon Carbide Reinforced
Aluminum Matrix Composites", Procedia
Engineering, 2014
2. V Mahesh Kumar, C V Venkatesh. "A
comprehensive review on material selection,
processing, characterization and applications of
aluminium metal matrix composites", Materials
Research Express, 2019
3. C. Kannan, R. Ramanujam. "Comparative study
on the mechanical and microstructural
characterisation of AA 7075 nano and hybrid
nanocomposites produced by stir and squeeze
casting", Journal of Advanced Research, 2017
4. G. Ranjith Kumar, G. Rajyalakshmi, Vijaya Kumar
Manupati. "Surface Micro Patterning of
Aluminium Reinforced Composite through Laser
Peening", International Journal of
Manufacturing, Materials, and Mechanical
Engineering, 2017
5. Atrian, A., G. H. Majzoobi, M. H. Enayati, and H.
Bakhtiari. "Mechanical and microstructural
characterization of Al7075/SiC

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IRJET- Tensile Property and Hardness of Al-7075 Matrix Reinforced with Silicon Carbide Particles

  • 1. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 07 | July 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 1751 Tensile Property and Hardness of Al-7075 Matrix Reinforced with Silicon Carbide Particles Muhammed Muddassir1, S.B Mallur2 1Department of Mechanical Engineering, University B.D.T College of Engineering, Davanagere 2Professor and Chairman, University B.D.T College of Engineering, Davanagere ---------------------------------------------------------------------***---------------------------------------------------------------------- Abstract - Aluminium 7075 alloy as a matrix material and the silicon carbide as a reinforcement material have been used because it has potential applications in aerospace and aircraft industries because of its low weight to high strength ratio. It also used because it has high wear resistance and creep resistance property. The investigation about the tensile property and hardness of Al 7075 and silicon carbide is needed so that metal matrix composite fabricated for the aerospace and aircraft industries should be defect free. In this work Al 7075 is reinforced with 0, 5, 10, 15, 20 wt % of silicon carbide by stir casting method. The resulted casted specimens are tested to know the tensile property and hardness of the composite. Key words: Al 7075, Stir casting, Tensile Strength, Hardness. 1. INTRODUCTION The use of metal matrix composite as structural engineering material has more attention in current years. Because of their more strength to low weight ratio, and toughness at high temperature which makes them suitable for various applications. Whereas engineering materials like steel are used as MMC because of its superior stiffness and high mechanical strength compare to matrix alloys, but the major disadvantage is its poorer ductility and lesser fracture toughness. MMC have high tensile and compressive stresses by transfer and distributing the applied load from ductile matrix to the reinforcement material. The transfer of load takes place from matrix to reinforcement if it has interfacial bonds. Therefore appropriate selection of matrix material and reinforcement material with their properties and the method of fabrication selected which effect this bond will significantly influence the resulting MMC. 2. METHODOLOGY The current research is carrying out on Aluminium 7075 alloy which is reinforced with silicon carbide particles. For Al 7075 metal various weight percentage of silicon carbide is added by stir casting technique. Five samples each prepared for tensile test and Hardness test. Samples are prepared by varying the silicon carbide weight percentage as 0%, 5%, 10%, 15% and 20%. In this process initially silicon carbide powder is preheated at a temperature of 4000c for an hour in the muffle furnace. After this preheated silicon carbide powder is poured in to the molten aluminium at a temperature of 7500c.Degasifier and cover flux is added. Hexachloroethane (c2cl6) is used as a degasifier to remove the entrapped air and cover flux (45 % Nacl, 45% Kcl, and 10% NaF) is added to prevent oxidation losses of aluminium during melting this improves the yield of molten metal from the charge. The silicon carbide powder is mixed in the molten aluminium with the help of stirrer so that uniform supply of silicon carbide particles in molten aluminium can be achieved. Following stirring hold molten metal for 5minutes and then it is poured in to the suitable moulds. The moulds in which the molten metal is poured should be preheated in order to keep away from thermoelectric voltage arise due to huge differences in temperature, and not to decrease the repair life of the moulds or scratch the coating applied. After pouring allow the molten metal to solidify and then take out from the mould. Fig: 1: Muffle furnace Fig: 2: Pouring of Molten metal
  • 2. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 07 | July 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 1752 Fig: 3: Casted Specimens Fig: 4: Machined Specimens 3. EXPERIMENTATION Material Selection: Matrix Material: Al7075 is chosen as matrix material due to wide applications in many engineering sectors. Aluminium 7075 is an aluminium alloy with zinc as main alloying element. The Composition of Al7075 is shown in the Table. Table: 1: Composition of Al-7075 Material Zinc Mg Copper Titanium Wt % 5.6-6.1 2.1-2.5 1.2-1.6 <0.5 Reinforcement Materials Silicon carbide used as reinforcement material. The properties of silicon carbide are shown in the table below Table 2: Properties of Sic Mechanical Properties Values Melting Point 0C 1400 Flexural Strength Mpa 550 Hardness 2800 Density g/cm3 3.1 Fracture Toughness Mpa/m2 4.6 Poisson’s Ratio 0.14 Composition used for Metal Matrix Composite:- Table 3: Composition Sample Wt. of Al- 7075 Wt. of Sic Al-7075 with 0% Sic 240 g 0 g Al-7075 with 5% Sic 261 g 13.05 g Al-7075 with 10% Sic 234 g 23.4 g Al-7075 with 15% Sic 225 g 33.75 g Al-7075 with 20% Sic 235 g 47 g 4. Results and Discussions 4.1 Tensile Test: The tensile test specimen is ready with size according to ASTM standard E8. The specimen for tensile test is shown in figure 5. The tensile test is carry out in computerized tensometer. Fig: 5: Specimen on Tensometer Fig: 6: Tested Specimens Table: 4: Ultimate Tensile Strength (Mpa) Materials Ultimate Tensile Strength (Mpa) Al-7075 with 0% Sic 153.95 Al-7075 with 5% Sic 162.09 Al-7075 with 10% Sic 170.38 Al-7075 with 15% Sic 207.29 Al-7075 with 20% Sic 190.7
  • 3. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 07 | July 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 1753 Variation in Tensile Strength: Fig: 7: Comparison of Ultimate Tensile strength Fig: 8: Variation of Ultimate Tensile Strength Tensile test are perform on a Tensometer for 0, 5, 10, 15 and 20 wt% of SiC composite and the reading are tabulate. It was practical that tensile strength increase with the increases in wt% of SiC until 15 wt% after that it gradually decreases as shown in the above graph. From the above graphs it clears that for 15 wt% of SiC in Al-7075 has maximum ultimate tensile strength. Table: 5: % of Reduction in Area Materials Reduction Area % Al-7075 with 0% Sic 0.052 Al-7075 with 5% Sic 0.054 Al-7075 with 10% Sic 0.056 Al-7075 with 15% Sic 0.069 Al-7075 with 20% Sic 0.067 Fig: 9: % of Reduction in Area From the above table it’s clear that as the percentage of reinforcement i.e. Silicon Carbide, increase the reduction area percentage also increase until 15 wt% of Silicon Carbide then after this the percentage of reduction area decreases. 4.1 Hardness Test: The conflict of materials against surface indentation is termed as hardness. The micro hardness of composites evaluates the border bond strength among reinforcing particles and matrix. Experiment has been conduct by changeable weight fraction of SiC (0%, 5%, 10%, 15%, and 20%). Hardness is record and tabulate. Hardness test have been conduct on each sample by means of a load of 30 kgf and Pyramidal Diamond indenter whose faces are set at a 136 degree angle from one another. Dimension of impression prepared by indenter have been predict by microscope. The equivalent value of hardness (HV) was calculated from standard formula. Table: 6: Vickers Hardness Number (VHN) Materials Vickers Hardness Al-7075 with 0% Sic 274 Al-7075 with 5% Sic 347.62 Al-7075 with 10% Sic 365.68 Al-7075 with 15% Sic 385.18 Al-7075 with 20% Sic 375.24 Fig: 10: Comparison of VHN 0 50 100 150 200 250 Al 7075 + 0% Sic Al 7075 + 5% Sic Al 7075 + 10% Sic Al 7075 + 15% Sic Al 7075 + 20% Sic Ultimate Tensile Strength (Mpa) 153.95 162.09 170.38 207.29 190.7 0 50 100 150 200 250 Al 7075 + 0% Sic Al 7075 + 5% Sic Al 7075 + 10% Sic Al 7075 + 15% Sic Al 7075 + 20% Sic Ultimate Tensile Strength (Mpa) 2.069 1.7507 1.4324 1.114 1.2732 Al 7075 + 0% Sic Al 7075 + 5% Sic Al 7075 + 10% Sic Al 7075 + 15% Sic Al 7075 + 20% Sic Reducton Area %
  • 4. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 07 | July 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 1754 Above table show the Vickers hardness numbers of composite contain varying wt. % of SiC reinforcements. The chart shows that adding of SiC particles in Al7075 matrix composites enhance the hardness composite, when compare with unreinforced Al7075. When unreinforced Al7075 have Vickers hardness number (274), hardness rate increase with increase in SiC content and utmost hardness value obtained is (385.18) for 15 wt. % SiC reinforced Al7075 matrix. The existences of harder and well bonded SiC particles in Al7075 matrix that obstruct the movement of dislocation increase the hardness of composite. 5. CONCLUSIONS: In this experimental study, Aluminium 7075 is reinforced with varying silicon carbide content (0, 5, 10, 15, 20 wt %) be prepared by using stir casting manufacture method. Tensile strength and hardness of the ready samples is calculated. Base on the investigational results the following conclusion is made:- The adding of silicon carbide in the Aluminium 7075 matrix increases the tensile strength and Vickers hardness when compared with unreinforced Aluminium 7075. 15 wt % of silicon carbide content in Aluminium 7075 matrix composite the maximum tensile strength and hardness. From the outcome above, silicon carbide reinforced Aluminium 7075 matrix composite showed better tensile strength and hardness than the unreinforced Aluminium 7075. References: 1. Md. Habibur Rahman, H. M. Mamun Al Rashed. "Characterization of Silicon Carbide Reinforced Aluminum Matrix Composites", Procedia Engineering, 2014 2. V Mahesh Kumar, C V Venkatesh. "A comprehensive review on material selection, processing, characterization and applications of aluminium metal matrix composites", Materials Research Express, 2019 3. C. Kannan, R. Ramanujam. "Comparative study on the mechanical and microstructural characterisation of AA 7075 nano and hybrid nanocomposites produced by stir and squeeze casting", Journal of Advanced Research, 2017 4. G. Ranjith Kumar, G. Rajyalakshmi, Vijaya Kumar Manupati. "Surface Micro Patterning of Aluminium Reinforced Composite through Laser Peening", International Journal of Manufacturing, Materials, and Mechanical Engineering, 2017 5. Atrian, A., G. H. Majzoobi, M. H. Enayati, and H. Bakhtiari. "Mechanical and microstructural characterization of Al7075/SiC