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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 5204
Mechanical Behavior of Aluminium-7075 Reinforced with Boron-
Carbide (B4C) and Graphite (Gr) Synthesized by Stir Casting.
M D Umar1, Zeeshan Ali2, Meer Ashfaqwali3, Syed Mudasser Ul Huq4,Mohammed Irfan5,
Mohmmed sohail chowdary6
1,2Assistant Professor, Department of Mechanical Engineering, Navodaya Institute of Technology, Raichur-
584101, Karnataka, India
3,4,5,6UG Scholar, Department of Mechanical Engineering, Navodaya Institute of Technology, Raichur-584101,
Karnataka, India
---------------------------------------------------------------------***----------------------------------------------------------------------
Abstract - The paper is the result of investigations made on microstructure and mechanical behavior of Al7075, Al7075-4% B4C,
Al7075-4% Graphite and Al7075-4% B4C+4% Graphite. The microstructure of the compositeswasexaminedbyscanningelectron
microscopy. Further, mechanical behavior of composites was studied. Mechanical properties like hardness, ultimate tensile
strength; yield strength were evaluated as per ASTM standards. Microstructural observation revealed uniform distribution of
reinforcement particles in the matrix. The analysis disclosed hardness, ultimate tensile strength, and yield strength of composites
increased due to addition of reinforcements.
Key Words: Composites, Al-7075, B4C, Gr, Microstructure, Tribological Behaviour.
1. INTRODUCTION
As there a trend in advancement in the technology there is more demand for the materials which saves energy in the areasof
aerospace and also light weight and economical and in the areas of defense, aviation, automation, and many of the aircraft
industries. So major applications are about Reducing Weight and also maintaining the mechanical and other tribological
properties improves because of which composites of Aluminium are found most suitable.Aluminiumisapplicable becauseitis
corrosion resistance material also when its layer reacts with air to form oxides on surface which offers resistance to the metal
erosion due to the rubbing action against two surfaces in an application. Hence it widely used in the applications of aerospace
which don’t have considerable wear resistance by itself. Therefore, there is need for development in the properties is much
needed.
Al-7075 is alloys of which contains zinc as their major alloying element, and is combined with copper and magnesium.
Aluminum alloys got highest strength in comparison with other alloys. As these are wrought alloys secondary machining is
possible. When further heat treatment is done it has highest mechanical strength. Aluminium alloys used in manufacturing of
automotive components and various aircraft structures (extrusions, forgings, sheets). These also found in high stressed parts
fabrication.
1.1 Materials
Al-7075 is an alloy with zinc as the primary alloying element. It has good strength comparable to many sheets of steel and
average machinability but has high resistance to corrosion than many other aluminium alloys. It’s relatively high-cost limits
and used in applications where cheaper alloys are not suitable.
Table1. Chemical Composition of Aluminium alloy
Element
Content
(%)
Aluminum, Al 90
Zinc, Zn 5.6
Magnesium, Mg 2.5
Copper, Cu 1.6
Chromium, Cr 0.23
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 5205
1.2 Preparation of Aluminium alloy Composites
The stir casting method was used develop the reinforcement metal matrix composites with the temperature of stir casting
furnace was maintained at 7000C. AL 7075 is first put into the crucible and furnace is closed. After twenty minutes, the metals
were verified for their molten state and after the confirmation, the metals such as boron carbide and graphite were put inside
and the furnace was closed. After 15 to 20 minutes, the boron carbide and graphite was added and the aluminium stirrer was
set to 550 rpm and it rotates. After the stirrer is rotated for about five minutes, the stirrer was stopped and the molten metal
was taken out. It was kept in cooling nature for about two hours.
Base Material B4C (%) Gr (%) Stir Speed
(rpm)
Stir Time
(mins)
Pouring
Temp. (C)
Preheated
Temp. (C)
Al-7075 4 4 550 5 700 350
2. Testing of Composites
Microstructure study has been carried out on the prepared compositeusingVegasTescanmadescanningelectron microscope.
Basically the test samples of 10-12mm in diameter are cut from the prepared castings using lathe machine and are polished
thoroughly as already mention methods it is etched using reagent for better results. The polished specimens which looks like
mirror. The specimens are characterized for various magnifications (100X, 200X, 800X) to indicate distribution of
reinforcements in metal matrix. The microstructures of samples i.e. as cast, 4 wt% B4C and 4wt% of Graphite are also
examined.
Tensile test specimens were machined from the cast samples. Thetensilespecimensofcircularcrosssectionwitha diameterof
9 mm and gauge length of 45mm were prepared according to the ASTM E8 standard testing procedure using Instron made
Universal Testing Machine. All the tests were conducted in a displacement control modeata rateof0.1mm/min.Multipletests
were conducted and the best results were averaged. Various tensilepropertieslikeultimatetensilestrength,yieldstrength and
percentage elongation were evaluated for as cast Aluminium alloy.Figure1showingthetensiletestspecimendimensionsused
to conduct the experiments.
Figure 1: Tensile specimen and its dimensions in mm
Results and Discussion
Microstructure Study
(a) (b)
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 5206
(c) (d)
Figure 2: Showing the Scanning Electron Microscope image of Al-7075alloy(a) and 4%B4C+4%Gr (b)
Figure 2 (a) shows the SEM microphotographs of Aluminium alloy as cast. Fig. 2 (b) clearly showsandevendistributionof B4C
in the Aluminium alloy matrix. similarly ,Fig 2 (c) clearly shows and even distribution of Gr and Fig 2 (d) clearly shows and
even distribution of Aluminium with 4 wt. % B4C+4%Gr particulate. There is no evidence of casting defects such as porosity,
shrinkages, slag inclusion and cracks which is indicative of sound castings. In this, wetting effect betweenparticlesandmolten
Aluminium alloy matrix also retards the movement of the reinforcement thus, the particles can remain suspended for a long
time in the melt leading to uniform distribution.
Figure 3: Eneregy Dispersive Spectrograph of Aluminium Alloy
Figure 3: Eneregy Dispersive Spectrograph of Hybrid Aluminium Alloy
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 5207
In order to confirm the presence of B4C+4%Gr energy dispersive spectroscope analysis was carried out at the edge of the
reinforcement particle and Aluminium alloy matrix. The EDSspectrumrevealsthepresenceofAl,Zn,CuandMgintheinterface
reaction layer.
Tensile Properties
After the test is completed the results are taken on an average and mentioned. We see that the values are increasing as weadd
the reinforcements to the aluminium alloy. We achieve a maximum tensilestressof248.88MPa forHybridcompositematerial.
We can easily make out the difference that upon addition ofreinforcementsthereisgradual increaseintrendforyieldstrength.
This is because reinforcements act as obstacles to the moment of dislocations and also upon adding the Graphite into molten
metal it increases the elongation properties there by yielding more which in turn yield strength increased.
212.45
226.49 226.36
248.88
190
200
210
220
230
240
250
260
Al7075 Al7075-4%B4C Al7075-4%Graphite Al7075-4%B4C+4%
Graphite
StressinMPa
UltimateTensile Strength
Figure 4a: Ultimate tensile strength of Hybrid Aluminium alloy composites
172.34
189.38 185.26
198.46
150
160
170
180
190
200
210
Al7075 Al7075-4% B4C Al7075-4% Graphite Al7075-4% B4C+4%
Graphite
StressinMPa
Yield Strength
Figure 4b: Yield strength of Hybrid Aluminium alloy composites.
Hardness Study
The Brinell hardness test on all compositions was conducted using steel ball indenter at an applied load of 60kgffortimeof 10
seconds to each sample at different locations. We can see that the hardness values are greater than that of its aluminiumalloy.
It is clear that hardness values are decreasing due to graphite contenting the alloy. Drop of hardness values due to softness of
the graphite, which is soft do not contribute for hardness of the composite as they won’t act as barriers for the dislocations
moment within the matrix but Boron Carbides does contrary; since B4C particles which are ceramics having much higher
hardness than the base matrix, they obstruct dislocations. The observations made are consistent Increased in the hardness of
composites reinforced with B4C and Gr has been reported by several workers.
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 5208
69.6
78.2
66.5
79.6
55
60
65
70
75
80
85
Al7075 Al7075-4% B4C Al7075-4% Graphite Al7075-4% B
Graphit
BrinellHardnessNumber
Hardness
Figure 5: Hardness of Hybrid Aluminium alloy composites
3. CONCLUSIONS
The mechanical investigations of the Aluminium alloy composites materials produced by stir castingareremarkedas
below:
 The liquid metallurgy technique was successfully adopted in the preparation of Aluminium alloy composites.
 The microstructural studies revealed the uniform distribution of the B4C and Gr particulates in the Aluminium
alloy matrix.
 The ultimate tensile strength and yield strength properties of the composites found to be higher thanthatofbase
matrix.
 Improvements in hardness of the Aluminium alloy matrix were obtained with the addition of B4C and Gr
particulates.
REFERENCES
[1] Kenneth Kanayo Alaneme and Kazeem OladitiSanusi, EngineeringScienceandTechnology,anInternational Journal, 18(3),
416(2015)
[2] S. Nallusamy and A. Karthikeyan, Indian Journal of Science and Technology, 9(35), 01(2016)
[3] A. Karthikeyan and S. Nallusamy, Int. Journal of Engineering Research in Africa, 31, 36(2017)
[4] Viney Kumara, Rahul Dev Guptab and N.K. Batrab, Procedia Materials Science, 6, 1365(2014)
[5] S. Nallusamy and Gautam Majumdar, Int. Journal of Performability Engg., 12(3), 229(2016)
[6] R. Suganthini Rekha, S. Nallusamy,R.VijayakumarandS.Saravanan, International Journal ofAppliedEngineering Research,
10(62), 133(2015)
[7] G. Ramanan, Dhas, Ramachandran and Samuel, Rasayan Journal of Chemistry, 10(2), 375(2017)
[8] S. Nallusamy and A. Karthikeyan, Journal of Nano Research, 49, 01(2017)
[9] Rajesh Prabha, N and Edwin Raja Dhas, J, Rasayan Journal of Chemistry, 10(3), 729(2017)
[10] S. Nallusamy and Saurabh Kumar, Indian Journal of Science and Technology, 9(16), 01(2016) 11. S. Jeevanantham, N.M.
Sivaram, D.S. Robinson Smart, S. Nallusamy and N. Manikanda Prabu.

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IRJET- Mechanical Behavior of Aluminium-7075 Reinforced with Boron-Carbide (B4C) and Graphite (GR) Synthesized by Stir Casting

  • 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 5204 Mechanical Behavior of Aluminium-7075 Reinforced with Boron- Carbide (B4C) and Graphite (Gr) Synthesized by Stir Casting. M D Umar1, Zeeshan Ali2, Meer Ashfaqwali3, Syed Mudasser Ul Huq4,Mohammed Irfan5, Mohmmed sohail chowdary6 1,2Assistant Professor, Department of Mechanical Engineering, Navodaya Institute of Technology, Raichur- 584101, Karnataka, India 3,4,5,6UG Scholar, Department of Mechanical Engineering, Navodaya Institute of Technology, Raichur-584101, Karnataka, India ---------------------------------------------------------------------***---------------------------------------------------------------------- Abstract - The paper is the result of investigations made on microstructure and mechanical behavior of Al7075, Al7075-4% B4C, Al7075-4% Graphite and Al7075-4% B4C+4% Graphite. The microstructure of the compositeswasexaminedbyscanningelectron microscopy. Further, mechanical behavior of composites was studied. Mechanical properties like hardness, ultimate tensile strength; yield strength were evaluated as per ASTM standards. Microstructural observation revealed uniform distribution of reinforcement particles in the matrix. The analysis disclosed hardness, ultimate tensile strength, and yield strength of composites increased due to addition of reinforcements. Key Words: Composites, Al-7075, B4C, Gr, Microstructure, Tribological Behaviour. 1. INTRODUCTION As there a trend in advancement in the technology there is more demand for the materials which saves energy in the areasof aerospace and also light weight and economical and in the areas of defense, aviation, automation, and many of the aircraft industries. So major applications are about Reducing Weight and also maintaining the mechanical and other tribological properties improves because of which composites of Aluminium are found most suitable.Aluminiumisapplicable becauseitis corrosion resistance material also when its layer reacts with air to form oxides on surface which offers resistance to the metal erosion due to the rubbing action against two surfaces in an application. Hence it widely used in the applications of aerospace which don’t have considerable wear resistance by itself. Therefore, there is need for development in the properties is much needed. Al-7075 is alloys of which contains zinc as their major alloying element, and is combined with copper and magnesium. Aluminum alloys got highest strength in comparison with other alloys. As these are wrought alloys secondary machining is possible. When further heat treatment is done it has highest mechanical strength. Aluminium alloys used in manufacturing of automotive components and various aircraft structures (extrusions, forgings, sheets). These also found in high stressed parts fabrication. 1.1 Materials Al-7075 is an alloy with zinc as the primary alloying element. It has good strength comparable to many sheets of steel and average machinability but has high resistance to corrosion than many other aluminium alloys. It’s relatively high-cost limits and used in applications where cheaper alloys are not suitable. Table1. Chemical Composition of Aluminium alloy Element Content (%) Aluminum, Al 90 Zinc, Zn 5.6 Magnesium, Mg 2.5 Copper, Cu 1.6 Chromium, Cr 0.23
  • 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 5205 1.2 Preparation of Aluminium alloy Composites The stir casting method was used develop the reinforcement metal matrix composites with the temperature of stir casting furnace was maintained at 7000C. AL 7075 is first put into the crucible and furnace is closed. After twenty minutes, the metals were verified for their molten state and after the confirmation, the metals such as boron carbide and graphite were put inside and the furnace was closed. After 15 to 20 minutes, the boron carbide and graphite was added and the aluminium stirrer was set to 550 rpm and it rotates. After the stirrer is rotated for about five minutes, the stirrer was stopped and the molten metal was taken out. It was kept in cooling nature for about two hours. Base Material B4C (%) Gr (%) Stir Speed (rpm) Stir Time (mins) Pouring Temp. (C) Preheated Temp. (C) Al-7075 4 4 550 5 700 350 2. Testing of Composites Microstructure study has been carried out on the prepared compositeusingVegasTescanmadescanningelectron microscope. Basically the test samples of 10-12mm in diameter are cut from the prepared castings using lathe machine and are polished thoroughly as already mention methods it is etched using reagent for better results. The polished specimens which looks like mirror. The specimens are characterized for various magnifications (100X, 200X, 800X) to indicate distribution of reinforcements in metal matrix. The microstructures of samples i.e. as cast, 4 wt% B4C and 4wt% of Graphite are also examined. Tensile test specimens were machined from the cast samples. Thetensilespecimensofcircularcrosssectionwitha diameterof 9 mm and gauge length of 45mm were prepared according to the ASTM E8 standard testing procedure using Instron made Universal Testing Machine. All the tests were conducted in a displacement control modeata rateof0.1mm/min.Multipletests were conducted and the best results were averaged. Various tensilepropertieslikeultimatetensilestrength,yieldstrength and percentage elongation were evaluated for as cast Aluminium alloy.Figure1showingthetensiletestspecimendimensionsused to conduct the experiments. Figure 1: Tensile specimen and its dimensions in mm Results and Discussion Microstructure Study (a) (b)
  • 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 5206 (c) (d) Figure 2: Showing the Scanning Electron Microscope image of Al-7075alloy(a) and 4%B4C+4%Gr (b) Figure 2 (a) shows the SEM microphotographs of Aluminium alloy as cast. Fig. 2 (b) clearly showsandevendistributionof B4C in the Aluminium alloy matrix. similarly ,Fig 2 (c) clearly shows and even distribution of Gr and Fig 2 (d) clearly shows and even distribution of Aluminium with 4 wt. % B4C+4%Gr particulate. There is no evidence of casting defects such as porosity, shrinkages, slag inclusion and cracks which is indicative of sound castings. In this, wetting effect betweenparticlesandmolten Aluminium alloy matrix also retards the movement of the reinforcement thus, the particles can remain suspended for a long time in the melt leading to uniform distribution. Figure 3: Eneregy Dispersive Spectrograph of Aluminium Alloy Figure 3: Eneregy Dispersive Spectrograph of Hybrid Aluminium Alloy
  • 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 5207 In order to confirm the presence of B4C+4%Gr energy dispersive spectroscope analysis was carried out at the edge of the reinforcement particle and Aluminium alloy matrix. The EDSspectrumrevealsthepresenceofAl,Zn,CuandMgintheinterface reaction layer. Tensile Properties After the test is completed the results are taken on an average and mentioned. We see that the values are increasing as weadd the reinforcements to the aluminium alloy. We achieve a maximum tensilestressof248.88MPa forHybridcompositematerial. We can easily make out the difference that upon addition ofreinforcementsthereisgradual increaseintrendforyieldstrength. This is because reinforcements act as obstacles to the moment of dislocations and also upon adding the Graphite into molten metal it increases the elongation properties there by yielding more which in turn yield strength increased. 212.45 226.49 226.36 248.88 190 200 210 220 230 240 250 260 Al7075 Al7075-4%B4C Al7075-4%Graphite Al7075-4%B4C+4% Graphite StressinMPa UltimateTensile Strength Figure 4a: Ultimate tensile strength of Hybrid Aluminium alloy composites 172.34 189.38 185.26 198.46 150 160 170 180 190 200 210 Al7075 Al7075-4% B4C Al7075-4% Graphite Al7075-4% B4C+4% Graphite StressinMPa Yield Strength Figure 4b: Yield strength of Hybrid Aluminium alloy composites. Hardness Study The Brinell hardness test on all compositions was conducted using steel ball indenter at an applied load of 60kgffortimeof 10 seconds to each sample at different locations. We can see that the hardness values are greater than that of its aluminiumalloy. It is clear that hardness values are decreasing due to graphite contenting the alloy. Drop of hardness values due to softness of the graphite, which is soft do not contribute for hardness of the composite as they won’t act as barriers for the dislocations moment within the matrix but Boron Carbides does contrary; since B4C particles which are ceramics having much higher hardness than the base matrix, they obstruct dislocations. The observations made are consistent Increased in the hardness of composites reinforced with B4C and Gr has been reported by several workers.
  • 5. 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 5208 69.6 78.2 66.5 79.6 55 60 65 70 75 80 85 Al7075 Al7075-4% B4C Al7075-4% Graphite Al7075-4% B Graphit BrinellHardnessNumber Hardness Figure 5: Hardness of Hybrid Aluminium alloy composites 3. CONCLUSIONS The mechanical investigations of the Aluminium alloy composites materials produced by stir castingareremarkedas below:  The liquid metallurgy technique was successfully adopted in the preparation of Aluminium alloy composites.  The microstructural studies revealed the uniform distribution of the B4C and Gr particulates in the Aluminium alloy matrix.  The ultimate tensile strength and yield strength properties of the composites found to be higher thanthatofbase matrix.  Improvements in hardness of the Aluminium alloy matrix were obtained with the addition of B4C and Gr particulates. REFERENCES [1] Kenneth Kanayo Alaneme and Kazeem OladitiSanusi, EngineeringScienceandTechnology,anInternational Journal, 18(3), 416(2015) [2] S. Nallusamy and A. Karthikeyan, Indian Journal of Science and Technology, 9(35), 01(2016) [3] A. Karthikeyan and S. Nallusamy, Int. Journal of Engineering Research in Africa, 31, 36(2017) [4] Viney Kumara, Rahul Dev Guptab and N.K. Batrab, Procedia Materials Science, 6, 1365(2014) [5] S. Nallusamy and Gautam Majumdar, Int. Journal of Performability Engg., 12(3), 229(2016) [6] R. Suganthini Rekha, S. Nallusamy,R.VijayakumarandS.Saravanan, International Journal ofAppliedEngineering Research, 10(62), 133(2015) [7] G. Ramanan, Dhas, Ramachandran and Samuel, Rasayan Journal of Chemistry, 10(2), 375(2017) [8] S. Nallusamy and A. Karthikeyan, Journal of Nano Research, 49, 01(2017) [9] Rajesh Prabha, N and Edwin Raja Dhas, J, Rasayan Journal of Chemistry, 10(3), 729(2017) [10] S. Nallusamy and Saurabh Kumar, Indian Journal of Science and Technology, 9(16), 01(2016) 11. S. Jeevanantham, N.M. Sivaram, D.S. Robinson Smart, S. Nallusamy and N. Manikanda Prabu.