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International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 06 | June 2019 www.irjet.net p-ISSN: 2395-0072
© 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 2717
"Characterization of Aluminum 7085/WC/Fly Ash Hybrid Composites for
Vibration Applications"
Mr Shivakumar V Aravatagimath, Prof Prashant S Patil
----------------------------------------------------------------------***-----------------------------------------------------------------------
Abstract - The present work on preparation of fly ash and tungsten carbide reinforced AA 7085composites by stir casting and
characteristic evaluation of characteristics
AA 7085/WC/Fly ash composites are fabricated with fairly uniform dispersions en-route the process of stir casting.
•The microstructure of the fabricated composites were analyzed using a typical SEM which revealed uniform dispersion of
reinforced particulates with strong bonding between the aluminum 7085 and particulates.
•The tensile strength improved from 245.8426 MPa to 314.026 MPa, while the yield strength enhanced from 176.312 MPa to
234.02 MPa, percentage elongation reduced from 9.22 to 3.64, the improvement in tensile strength is due to the addition of
tungsten carbide reinforcement particles which enhances the tensile characteristics. There is substantial increase in tensile
strength of C7composites when compared with ‘C1’ Specimen. The ductility of the composite specimens reduces with the increase
in strength and thus the C7 composites exhibit a reduced ductility as compared to C1 composite specimen. The percentage
elongation of the MMC’s decreased with increase in tungsten carbide and flyash content, which confirmed that tungsten carbide
addition increased brittleness.
•The compressive strength increased from 1274.2 MPa to 1522.02 MPa, while % reduction dropped down from 6.56 to 2.34, this is
majorly due to the bonding of reinforcements with the matrix phase that will ultimately enhance its ability to resist compression.
From current investigations and critical inferences of the given work, there is a vast scope for future researching the following
areas.
 Detailed wear characterization can be carried out.
 Corrosion studies can be carried out.
 Dynamic loading analysis can be done.
 Results can be correlated using analysis packages.
 Detailed characterization of the process methodologies can be carried out effectively.
Key Words: Stir Casting Technique, Universal Testing Machine, Lathe Machine, Brinell Harness Testing Machine
1. INTRODUCTION: Current Engineering applications require materials that are more grounded, lighter and progressively
moderate. Real research for the progression of materials that have extraordinary solidarity to weight extent and are sensible
for vehicle applications are picking up significance. In-advantage of execution demands for some propelled material systems, a
wide scope of properties which are difficult to meet using solid materials is accomplished on the way composite materials.
Metal framework composites are famed to promise such uniquely fitted a thing essential in a huge extent of structure uses. A
part of things mixes incorporates large unequivocal quality, less warm coefficients, large wear opposition, extraordinary
reducing limits, high express robustness and appealing components of disintegration check.
Generally, one section goes about as a grid in which the fortifying stage is strengthened. The framework part is as such, the
heap bearing stage, while the support is the heap exchanging stage. Right when the system part is metal, we consider such a
composite a metal network composite (MMC). The help can be particulates, short fibers or constant fiber. There are three
components that choose the characteristics of a composite which are support, system, and interface. The activity of the system
was seen as that of a medium or cover to hold the strong and firm fibers or various types of reinforcements. Consistently,
regardless, we can understand that the execution of the composite material will be always affected by the mechanical
structure and its characteristics. It is particularly legitimate for the MMC in light of the fact that the explicit showing of
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 06 | June 2019 www.irjet.net p-ISSN: 2395-0072
© 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 2718
solidifying a fortress can result in changes in the fine structure of the metallic cross-section and, hence in their structure fragile
properties. The undertakings to make financially engaging composite portions have achieved a couple of innovative
assembling methodologies right presently being used in the car and aviation spaces. It is plainly obvious, especially for
composites, that the improvement in manufacture approach alone isn't adequate to crush the cost acceleration. It is essential
that there be an organized upgrade in fabrication, attributes, tooling, quality confirmation, for composites
2. METHODOLOGY
2.1 Methodology Adopted
2.2 PROCESSING TECHNIQUE: Processing technique is important to synthesize fly ash and tungsten carbide reinforced
composites, the main purpose of many research and experiments is to enhance circulation of reinforcements in composite
materials & also improve the bonding between reinforcements and matrix phase. Also chemical reaction should be avoided
during the process of fabrication of composites.
2.3Experimental setup for stir casting technique:
Vibration Characterization
2.4 TESTS CONDUCTED: The various tests conducted to evaluate the characteristics of the composite materials are
herewith presented below:
 Tensile Tests
 Compression Tests
 Hardness Tests
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 06 | June 2019 www.irjet.net p-ISSN: 2395-0072
© 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 2719
2.5 VIBRATION TESTS:
The vibration tests were accomplished in a vibration test setup fitted with a FFT analyzer, it comprises of a data logger
connected to the system interface configured using a Lab VIEW software. The test setup comprises of a cantilever arrangement
to which the composite plates are mounted and excited using excitation hammers connected to the accelerometers that takes
note of the reading in the system, the arrangement of this setup is as shown in below figure.
2.5 RESULTS AND DISCUSSION:
Results of Ultimate Tensile Strength
Results of Yield Strength
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 06 | June 2019 www.irjet.net p-ISSN: 2395-0072
© 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 2720
Results of % Elongation
Results of Compression Strength (MPa)
Results of % Reduction
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 06 | June 2019 www.irjet.net p-ISSN: 2395-0072
© 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 2721
2.6 CONCLUSIONS
The present work on preparation of fly ash and tungsten carbide reinforced AA 7085composites by stir casting and
characteristic evaluation of characteristics has led to following conclusions.
• AA 7085/WC/Fly ash composites are fabricated with fairly uniform dispersions en-route the process of stir casting.
• The microstructure of the fabricated composites were analyzed using a typical SEM which revealed uniform
dispersion of reinforced particulates with strong bonding between the aluminum 7085 and particulates.
• The tensile strength improved from 245.8426 MPa to 314.026 MPa, while the yield strength enhanced from 176.312
MPa to 234.02 MPa, percentage elongation reduced from 9.22 to 3.64, the improvement in tensile strength is due to the
addition of tungsten carbide reinforcement particles which enhances the tensile characteristics. There is substantial increase
in tensile strength of C7composites when compared with ‘C1’ Specimen. The ductility of the composite specimens reduces with
the increase in strength and thus the C7 composites exhibit a reduced ductility as compared to C1 composite specimen. The
percentage elongation of the MMC’s decreased with increase in tungsten carbide and flyash content, which confirmed that
tungsten carbide addition increased brittleness.
Results of Hardness Test
FRF Modal data of the composite specimens
Results of modal frequency analysis
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 06 | June 2019 www.irjet.net p-ISSN: 2395-0072
© 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 2722
• The compressive strength increased from 1274.2 MPa to 1522.02 MPa, while % reduction dropped down from 6.56 to
2.34, this is majorly due to the bonding of reinforcements with the matrix phase that will ultimately enhance its ability to resist
compression.
• The hardness enhanced from 82.96 to 105.46, this increase in characteristic property is due to the fact that the micro
titanium reinforcements resist the movement of dislocations within the matrix. An improvement in hardness is observed for
C7composites when compared with C1 Specimen.
• The vibration analysis carried out has herewith validated that the composite specimen fabricated has the capability to
damp the vibrations and the results of analytical simulations carried out using ANSYS software has proved it. Further, the
damping ratio varies for different modal shapes from 0.157 e-3 to 2.180 e – 3 for C7 composite specimen, this shows an
incremental enhancement in the vibration characteristics as compared to the base Aluminum 7085 alloy, since the damping
ratio for aluminum 7085 alloy validated from the ASTM data hand book predicts the values for damping ratio to vary from 0.4
(e-4) to 0.4 (e-3). Also the amplitude of vibration is reduced for varying frequency with the addition of reinforcements.
REFERENCES:
1- Surappa.M.K “Aluminium Matrix Composites: Challenges and Opportunities,”
2- Raj Kumar,., Microwave sintering of Al–graphite composites,
3- S. Naher, D. Brabazon, L. Looney “Simulation of the Stir Casting Process” journal of material processing Technology 143–144
(2003) 567–571.
4- Tjong S C, Material. Science. Engg.
5- S. Suresh, N. Shenbaga Vinayaga Moorthi, S.C. Vettivel, N. Selvakumar ; “Process development in stir Casting and
investigation on microstructures and wear behavior of TiB2 on Al6061 MMC”; Materials And Design 59 by elsevier (2014),
383–396.
6- Shubham Mathur, Alok Barnawal; “Effect of Process Parameter of Stir Casting on Metal Matrix Composites”; International
Journal of Science and Research (IJSR) (2013), 395-398.
7- H. Sun Ph.D., J. E. Orth Ph.D., H. G. Wheat Ph.D.; “ Corrosion Behavior of Aluminum based Metal Matrix Composite”, Journal of
JOM; Volume 45, Issue 9, pp 36-41.
8- Riccardo Casati and Maurizio Vedani; “Metal Matrix Composites Reinforced by Nano -Particles”, Journal of Metals (2014),
Vol. 4, pp. 65-83.
9- Wang, Jinyong; Li, Yan; Jiang, "Fabrication of Ultralong and Electrically Uniform Single-Walled Carbon Nanotubes on Clean
Substrates".
10- "Legendary Swords' Sharpness, Strength From Nanotubes, Study Says".
11- "Nanotechnology: A Guide to Nano-Objects" by, M.S,Wong. (2011).
12-F.Wan, M. Abdel hameed “Preparation and Characteristics of Cu-Al2O3nanocomposite”.
13- Kumar Jatinder, Hari Singh, “Production Technologies of Metal Matrix Composite
14-Prabhakar Rao, PK Jayashree, “Review on Effect of Aluminum on Stir Cast Aluminum Metal Matrix Composites”.
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 06 | June 2019 www.irjet.net p-ISSN: 2395-0072
© 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 2723
BIOGRAPHIES
Shivakumar V Aravatagimath,
M.Tech (Machine Design)
B.L.D.E.A’s V. P. Dr.P.G.H College
of Engineering and Technology,
Vijayapur, Karnataka, India
Prof.P.S.Patil
Asst. Professor,
Dept. of Mechanical Engineering,
B.L.D.E.A’s V. P. Dr.P.G.H College
of Engineering and Technology,
Vijayapur, Karnataka, India

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Characterization of Aluminum 7085 composites

  • 1. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 06 | June 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 2717 "Characterization of Aluminum 7085/WC/Fly Ash Hybrid Composites for Vibration Applications" Mr Shivakumar V Aravatagimath, Prof Prashant S Patil ----------------------------------------------------------------------***----------------------------------------------------------------------- Abstract - The present work on preparation of fly ash and tungsten carbide reinforced AA 7085composites by stir casting and characteristic evaluation of characteristics AA 7085/WC/Fly ash composites are fabricated with fairly uniform dispersions en-route the process of stir casting. •The microstructure of the fabricated composites were analyzed using a typical SEM which revealed uniform dispersion of reinforced particulates with strong bonding between the aluminum 7085 and particulates. •The tensile strength improved from 245.8426 MPa to 314.026 MPa, while the yield strength enhanced from 176.312 MPa to 234.02 MPa, percentage elongation reduced from 9.22 to 3.64, the improvement in tensile strength is due to the addition of tungsten carbide reinforcement particles which enhances the tensile characteristics. There is substantial increase in tensile strength of C7composites when compared with ‘C1’ Specimen. The ductility of the composite specimens reduces with the increase in strength and thus the C7 composites exhibit a reduced ductility as compared to C1 composite specimen. The percentage elongation of the MMC’s decreased with increase in tungsten carbide and flyash content, which confirmed that tungsten carbide addition increased brittleness. •The compressive strength increased from 1274.2 MPa to 1522.02 MPa, while % reduction dropped down from 6.56 to 2.34, this is majorly due to the bonding of reinforcements with the matrix phase that will ultimately enhance its ability to resist compression. From current investigations and critical inferences of the given work, there is a vast scope for future researching the following areas.  Detailed wear characterization can be carried out.  Corrosion studies can be carried out.  Dynamic loading analysis can be done.  Results can be correlated using analysis packages.  Detailed characterization of the process methodologies can be carried out effectively. Key Words: Stir Casting Technique, Universal Testing Machine, Lathe Machine, Brinell Harness Testing Machine 1. INTRODUCTION: Current Engineering applications require materials that are more grounded, lighter and progressively moderate. Real research for the progression of materials that have extraordinary solidarity to weight extent and are sensible for vehicle applications are picking up significance. In-advantage of execution demands for some propelled material systems, a wide scope of properties which are difficult to meet using solid materials is accomplished on the way composite materials. Metal framework composites are famed to promise such uniquely fitted a thing essential in a huge extent of structure uses. A part of things mixes incorporates large unequivocal quality, less warm coefficients, large wear opposition, extraordinary reducing limits, high express robustness and appealing components of disintegration check. Generally, one section goes about as a grid in which the fortifying stage is strengthened. The framework part is as such, the heap bearing stage, while the support is the heap exchanging stage. Right when the system part is metal, we consider such a composite a metal network composite (MMC). The help can be particulates, short fibers or constant fiber. There are three components that choose the characteristics of a composite which are support, system, and interface. The activity of the system was seen as that of a medium or cover to hold the strong and firm fibers or various types of reinforcements. Consistently, regardless, we can understand that the execution of the composite material will be always affected by the mechanical structure and its characteristics. It is particularly legitimate for the MMC in light of the fact that the explicit showing of
  • 2. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 06 | June 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 2718 solidifying a fortress can result in changes in the fine structure of the metallic cross-section and, hence in their structure fragile properties. The undertakings to make financially engaging composite portions have achieved a couple of innovative assembling methodologies right presently being used in the car and aviation spaces. It is plainly obvious, especially for composites, that the improvement in manufacture approach alone isn't adequate to crush the cost acceleration. It is essential that there be an organized upgrade in fabrication, attributes, tooling, quality confirmation, for composites 2. METHODOLOGY 2.1 Methodology Adopted 2.2 PROCESSING TECHNIQUE: Processing technique is important to synthesize fly ash and tungsten carbide reinforced composites, the main purpose of many research and experiments is to enhance circulation of reinforcements in composite materials & also improve the bonding between reinforcements and matrix phase. Also chemical reaction should be avoided during the process of fabrication of composites. 2.3Experimental setup for stir casting technique: Vibration Characterization 2.4 TESTS CONDUCTED: The various tests conducted to evaluate the characteristics of the composite materials are herewith presented below:  Tensile Tests  Compression Tests  Hardness Tests
  • 3. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 06 | June 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 2719 2.5 VIBRATION TESTS: The vibration tests were accomplished in a vibration test setup fitted with a FFT analyzer, it comprises of a data logger connected to the system interface configured using a Lab VIEW software. The test setup comprises of a cantilever arrangement to which the composite plates are mounted and excited using excitation hammers connected to the accelerometers that takes note of the reading in the system, the arrangement of this setup is as shown in below figure. 2.5 RESULTS AND DISCUSSION: Results of Ultimate Tensile Strength Results of Yield Strength
  • 4. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 06 | June 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 2720 Results of % Elongation Results of Compression Strength (MPa) Results of % Reduction
  • 5. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 06 | June 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 2721 2.6 CONCLUSIONS The present work on preparation of fly ash and tungsten carbide reinforced AA 7085composites by stir casting and characteristic evaluation of characteristics has led to following conclusions. • AA 7085/WC/Fly ash composites are fabricated with fairly uniform dispersions en-route the process of stir casting. • The microstructure of the fabricated composites were analyzed using a typical SEM which revealed uniform dispersion of reinforced particulates with strong bonding between the aluminum 7085 and particulates. • The tensile strength improved from 245.8426 MPa to 314.026 MPa, while the yield strength enhanced from 176.312 MPa to 234.02 MPa, percentage elongation reduced from 9.22 to 3.64, the improvement in tensile strength is due to the addition of tungsten carbide reinforcement particles which enhances the tensile characteristics. There is substantial increase in tensile strength of C7composites when compared with ‘C1’ Specimen. The ductility of the composite specimens reduces with the increase in strength and thus the C7 composites exhibit a reduced ductility as compared to C1 composite specimen. The percentage elongation of the MMC’s decreased with increase in tungsten carbide and flyash content, which confirmed that tungsten carbide addition increased brittleness. Results of Hardness Test FRF Modal data of the composite specimens Results of modal frequency analysis
  • 6. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 06 | June 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 2722 • The compressive strength increased from 1274.2 MPa to 1522.02 MPa, while % reduction dropped down from 6.56 to 2.34, this is majorly due to the bonding of reinforcements with the matrix phase that will ultimately enhance its ability to resist compression. • The hardness enhanced from 82.96 to 105.46, this increase in characteristic property is due to the fact that the micro titanium reinforcements resist the movement of dislocations within the matrix. An improvement in hardness is observed for C7composites when compared with C1 Specimen. • The vibration analysis carried out has herewith validated that the composite specimen fabricated has the capability to damp the vibrations and the results of analytical simulations carried out using ANSYS software has proved it. Further, the damping ratio varies for different modal shapes from 0.157 e-3 to 2.180 e – 3 for C7 composite specimen, this shows an incremental enhancement in the vibration characteristics as compared to the base Aluminum 7085 alloy, since the damping ratio for aluminum 7085 alloy validated from the ASTM data hand book predicts the values for damping ratio to vary from 0.4 (e-4) to 0.4 (e-3). Also the amplitude of vibration is reduced for varying frequency with the addition of reinforcements. REFERENCES: 1- Surappa.M.K “Aluminium Matrix Composites: Challenges and Opportunities,” 2- Raj Kumar,., Microwave sintering of Al–graphite composites, 3- S. Naher, D. Brabazon, L. Looney “Simulation of the Stir Casting Process” journal of material processing Technology 143–144 (2003) 567–571. 4- Tjong S C, Material. Science. Engg. 5- S. Suresh, N. Shenbaga Vinayaga Moorthi, S.C. Vettivel, N. Selvakumar ; “Process development in stir Casting and investigation on microstructures and wear behavior of TiB2 on Al6061 MMC”; Materials And Design 59 by elsevier (2014), 383–396. 6- Shubham Mathur, Alok Barnawal; “Effect of Process Parameter of Stir Casting on Metal Matrix Composites”; International Journal of Science and Research (IJSR) (2013), 395-398. 7- H. Sun Ph.D., J. E. Orth Ph.D., H. G. Wheat Ph.D.; “ Corrosion Behavior of Aluminum based Metal Matrix Composite”, Journal of JOM; Volume 45, Issue 9, pp 36-41. 8- Riccardo Casati and Maurizio Vedani; “Metal Matrix Composites Reinforced by Nano -Particles”, Journal of Metals (2014), Vol. 4, pp. 65-83. 9- Wang, Jinyong; Li, Yan; Jiang, "Fabrication of Ultralong and Electrically Uniform Single-Walled Carbon Nanotubes on Clean Substrates". 10- "Legendary Swords' Sharpness, Strength From Nanotubes, Study Says". 11- "Nanotechnology: A Guide to Nano-Objects" by, M.S,Wong. (2011). 12-F.Wan, M. Abdel hameed “Preparation and Characteristics of Cu-Al2O3nanocomposite”. 13- Kumar Jatinder, Hari Singh, “Production Technologies of Metal Matrix Composite 14-Prabhakar Rao, PK Jayashree, “Review on Effect of Aluminum on Stir Cast Aluminum Metal Matrix Composites”.
  • 7. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 06 | June 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 2723 BIOGRAPHIES Shivakumar V Aravatagimath, M.Tech (Machine Design) B.L.D.E.A’s V. P. Dr.P.G.H College of Engineering and Technology, Vijayapur, Karnataka, India Prof.P.S.Patil Asst. Professor, Dept. of Mechanical Engineering, B.L.D.E.A’s V. P. Dr.P.G.H College of Engineering and Technology, Vijayapur, Karnataka, India