Ijraset Journal For Research in Applied Science and Engineering Technology
Authors: Deepak Kumar, B.S Pabla
DOI Link: https://doi.org/10.22214/ijraset.2023.56173
Certificate: View Certificate
The result of different volume % of Silicon Nitride (Si3N4) in AA 8011 alloy fabricated through stir casting process & then tested for hardness, wear test. Energy Dispersive Spectroscopy (EDS), and Scanning Electron Microscopy (SEM) of these samples are done. It is found that the highest hardness and wear strength can be obtained with the addition of 80 ?m particle size of Si3N4 with 6% of its total volume fraction. This increase in the properties is due to the increase in density caused by the addition of Si3N4 reinforcement particles. SEM study also shows that the distribution of Si3N4 with the matrix material. The maximum hardness is obtained at 40.7 HV in sample 04 having 6% of Silicon Nitride (Si3N4) and 94% of Aluminium Alloy 8011, Similarly, maximum wear is recorded in the sample having 6% of Silicon Nitride (Si3N4) and 94% of Aluminium Alloy 8011when the load is 4kg and RPM is 1800. As compared to the AA8011 hardness of the composite with the addition of the silicon nitride increases, the wear and the coefficient of the friction decreases as compared to the AA8011, and the friction force remains almost same.
I. INTRODUCTION
Composite is a mixture of two or more materials that are (mixed or bonded) but on a microscopic level. Generally, composite material is composed of matrix (polymers, metals or ceramics) and reinforcement (fibres, particles, flakes and fillers). The matrix holds the reinforcement to form the desired shape on the other hand the reinforcement improves the overall mechanical properties of the matrix. The final material which is composite exhibits better strength than each of the individual materials which is used for making composite.
Kelly [1] defines very clearly that the composite should not be regarded simply as a combination of two materials. Going further; the combination has its different properties. In terms of strength or resistance to heat or some other quality, it is better than either of the components alone or radically different from either of them.
Table 01 – properties of Reinforcement, Matrix & Composite
Properties of Reinforcement |
Properties of Matrix |
Properties of Composite |
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II. CHARACTERISTICS OF THE COMPOSITES
Composites consist of one or more discontinuous phases embedded in a continuous phase. The discontinuous phase is usually harder and stronger than the continuous phase and is called the 'reinforcement ' or 'reinforcing material', whereas the continuous phase is term-led as the ‘matrix’. The properties of composites are strongly dependent on the properties of their constituent materials, their distribution and the interaction among them. The composite properties may be the volume fraction sum of the properties of the constituents or the constituents may interact in a synergistic way resulting in improved or better properties. Apart from the nature of the constituent materials, the geometry of the reinforcement (shape, size and size distribution) influences the properties of the composite to a great extent. The concentration distribution and orientation of the reinforcement also affect the properties. The shape of the discontinuous phase (which may be spherical, cylindrical, or rectangular cross sanctioned prisms or platelets), the size and size distribution (which controls the texture of the material) and volume fraction determine the interfacial area, which plays an important role in determining the extent of ·the interaction between the reinforcement and the matrix. Concentration, usually measured as volume or weight fraction, determines the contribution of a single constituent to the overall properties of the composites. It is not only the single most important parameter influencing the properties of the composites but also an easily controllable manufacturing variable used to alter its properties. The orientation of the reinforcement affects the isotropy of the system.
III. TESTING SETUP
In the present research, AA8011 is matrix material and Si3N4 is reinforcement material. AA 8011 is the form of sheets having 3mm as thickness and in the form of sheets and Si3N4 is the powder form having 80 micro size. AA8011 around 800 grams is measured for first casting. For the second casting 784 grams of AA8011 and Si3N4 16 grams were measured. For the third casting 768 grams of AA8011 and Si3N4 32 grams of are measured. For fourth casting 752 grams of AA8011 and Si3N4 48 grams is measured.
Table 02 – Weight Percentages of composite
Sample No. |
Composition of Weight percentage of composite |
|
|
AA8011 |
Si3N4 |
1 |
100% |
0% |
2 |
98% |
2% |
3 |
96% |
4% |
4 |
94% |
6% |
More than 6% of the reinforcement is not mixing well in the matrix material as it forms white powder with slag with fabrication technique as stir casting.
IV. SELECTION OF FABRICATION TECHNIQUE
The stir casting technique is considered the best technique for the fabrication of aluminium metal matrix composite. A stir casting machine in the General workshop in NIT Hamirpur is used in the present work to cast the samples.
V. STIR CASTING
Stir casting is a liquid-state method for the fabrication of composite materials, in which a dispersed phase is mixed with a molten matrix metal using mechanical stirring. The stir casting technique appears a promising technique for the production of metal matrix composite. In stir casting, we use the stirrer to agitate the molten metal matrix. The stirrer is generally made up of material which can withstand a higher melting temperature than matrix temperature.
Generally, a graphite stirrer is used in stir casting. The distribution of particles in molten metal is also affected by the velocity of the stirrer, the angle of the stirrer, vortices cone. The process parameters for stir stir-casting route are as under:
A. Silicon Nitride
Silicon Nitride has high thermal stability with strong optical nonlinearities for all-optical applications. It is white in colour having high-melting-point. It is very hard (8.5 on the mohs scale). Si3N4 is the most thermodynamically stable and commercially important of the silicon nitrides, and the term "silicon nitride" commonly refers to this specific composition. Silicon nitride is a chemical compound of the elements silicon and nitrogen.
Table 03– Properties of Silicon Nitride
Material Properties |
Silicon Nitride |
Young’s Modulus (GPa) |
270 |
Poisson Ratio |
0.27 |
Thermal Conductivity (W/cm/C) |
0.032 |
Specific Heat (J/gC) |
0.71 |
Electrical Resistivity (?cm) |
0.6 |
Diectric Constant |
7.5 |
Density (g/cm3) |
3.44 |
Coefficient of Thermal Expansion (/OC) |
2810x10-7 |
B. AA8011
In the present study, AA8011 was used as the matrix material. AA8011 has good strength, good fatigue strength and average machinability. It has superior stress corrosion resistance compared to other aluminium alloys. The melting point of AA8011 starts around 510 to 636 degrees celsius. It was acquired from M/S Ozair Tradelink Gujrat, India in the form of raw material reached via India Mart. The various alloying elements identified in AA8011 are Al, Zn, Mg, Fe, Si, Mn, Ti, Cr and Cu.
Table 04 – Properties of AA8011
Material Properties |
AA8011 |
Tensile Strength (MPa) |
110 |
Yield Strength (MPa) |
140 |
Young’s Modulus (GPa) |
69 |
Specific Heat (J/gC) |
0.9 |
Poisson Ratio |
0.33 |
Thermal Conductivity (W/cm/C) |
2.1 |
Density (g/cm3) |
2.8 |
Melting Completion (liquid) (OC) |
600 |
Table 05 – Properties of AA8011
Registered International designation |
Composition in Weight percentage |
||||||||||
Si |
Cu |
Fe |
Mg |
Mn |
Zn |
Cr |
Ti |
B |
Li |
Zr |
|
8011 |
.70 |
.10 |
.65 |
.05 |
.20 |
.10 |
.05 |
.08 |
- |
- |
- |
C. Hardness Test
The resistance of a material to indentation, deformation or penetration using such as abrasion, scratching, impact or wear is generally determined by hardness tests such as Rockwell, Brinell or Vickers. The hardness of the samples was measured by using a Mitutoyo HM 100 series micro hardness tester as shown in Fig 4.9. The hardness test was performed at NITTTR Chandigarh. The Vickers hardness tester was used for measuring the hardness of fabricated samples. A diamond indenter, in the form of a right pyramid with a square base at an angle of 136 between opposite faces, is forced into the material under load. A load of 1 kg was applied for 10 seconds and after that indenter was removed. The two diagonals of indentation left on the surface of the material after removal of the load were measured using a microscope and their mean calculated.
D. Wear Test
The pin-on-disc wear and friction tester is used to investigate the tribological properties of materials/coatings in sliding contact, such as wear and friction behaviour. A stationary pin and a revolving disc slide against one another. Normal load, rotating speed, and worn track diameter are the variables. Wear is calculated by first determining the linear measurement of the original dimensions (length, width and height of the original sample). The sample shall be fixed perpendicular to the flat EN 31 disc, such that the sample revolves around the disc centre. The sample is pressed against the disc at different loads. The two data sets of linear dimensions shall be converted into their respective volumes and subtracted to obtain the volume of specimen lost due to wear.
VI. MICROSTRUCTURAL ANALYSIS
SEM is a type of electron microscope that produces images of a sample by scanning the surface with a focused beam of electrons. The electrons interact with atoms in the sample, producing various signals that contain information about the surface topography and composition of the sample. The electron beam is scanned in a raster scan pattern and the position of the beam is combined with the detected signal to produce an image. SEM can achieve resolution better than 1 nanometre. The surfaces of the specimens were examined by SEM JEOL JSM-IT 100 shown in Fig. SEM was used to analyze the microstructure of surfaces. The EDS technique detects X-rays emitted from the sample during bombardment by an electron beam to characterize the elemental composition of the analyzed volume. EDS was used to analyze the composition of the specimens.
VII. RESULT AND DISCUSSION
The result of the present investigation entitled “CHARACTERIZATION OF THE ALUMINUM MATRIX COMPOSITE REINFORCED WITH SILICON NITRIDE (AA8011/SI3N4) SYNTHESIZED BY THE STIR CASTING ROUTE” are compiled and presented in different subsections:
A. Wear Test
The behaviour of material is determined while it detects a deformation, due to a change in temperature, frictional force or coefficient of friction by varying load, rpm and time. The wear properties can be evaluated from various graphs like wear-time, temperature time, coefficient of friction time, and frictional force time for different weight percentages of reinforcement in aluminium matrix composite.
The present investigation is carried out to study on mechanical and microstructural properties of silicon nitride-reinforced aluminium alloy composite. The microstructure analysis is done by SEM and EDS is used to check the composition of the composite. Hardness tests and wear tests are used to study the mechanical properties of the composite. A. Conclusion The following conclusions are drawn based on experimental work and analysis of results on AA8011/Si3N4 composite. 1) The hardness of composite with matrix material AA8011 & reinforcement Silicon Nitride increases with an increase in weight per cent ratio of reinforcement. 2) After the addition of reinforcement of more than 6% of the weight percentage of the composite it is difficult to add more reinforcement as with this fabrication technique it does not mix well and when mixing reaction occurs between AA-8011 and Silicon Nitride white colour powder is been produced which stays above the material and do not even mix with slag or the matrix material. 3) The wear increases slowly with the increase in the reinforcement percentage in the matrix material. 4) There is no change in the coefficient of friction with the addition of the reinforcement in the matrix material. 5) The maximum hardness is obtained at 40.7 HV at 6 wt.% of Si3N4. B. Limitations Of The Present Work The present work voids affected mechanical properties. The stirring of matrix and reinforcement was done at varying stirring speeds i.e. 200 to 400 rpm. C. Scope For Future Work The present work leaves a wide scope for future investigation to explore many other aspects of AA8011/ Si3N4 composite.
[1] Kelly, A. (1967) Sci. American 217, (B), 161. “ Experimental study on Mechanical Properties of Polymer based Hybrid Composite” Volume – 4, Issue -10, 2017, Pages – 10904-10912. [2] Berghezan, A. Nucleus, 8(5) 1966, (Nucleus A. Editeur, 1, rhe, Chalgrin, Paris, 16(e). [3] Van suchetclan, Philips Res. Repts. Vol. 27.1972, p . 28 “ Investigation on tensile and compressive properties of jute fiber reinforced epoxyresin composites” www.thefreelibrary.com/in. [4] B. Ashok Kumar, “Characterization of the Aluminium Matrix Composite Reinforced with Silicon Nitride (AA6061/Si3N4) Synthesized by the Stir Casting Route” Volume 2022, Article ID 8761865 [5] Mr. M. Tamilarasan, “A Study on Effect of SiC on Mechanical Properties of Aluminium 8011 Metal Matrix” e-ISSN: 2395-0056. [6] Devananthan G., “ Mechanical Characterization of Al 8011 Aluminium alloy reinforced with Silicon carbide and fly ash” Available online at: https://www.ijariit.com. [7] J. Fayomi, “Experimental study of ZrB2-Si3N4 on the microstructure, mechanical and electrical properties of high grade AA8011 metal matrix composites” journal homepage: http://www.elsevier.com/locate/jalcom.
Copyright © 2023 Deepak Kumar, B.S Pabla. This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
Paper Id : IJRASET56173
Publish Date : 2023-10-16
ISSN : 2321-9653
Publisher Name : IJRASET
DOI Link : Click Here