a) Why Al Matrix Selection?
Currently, researchers around the world are concentrating on aluminium since it is having excellent mechanical and corrosion properties along with low density. Aluminium composites have excellent thermal properties, so it is extensively used in aerospace, automotive and avionics fields. Titanium finds extensive applications in aerospace engines because of its high temperature resistance, primarily for blades and compressor discs [7]. The literature work carried out shows that maximum published work has focused on aluminium-based composites thru the following advantages: extensive variety of alloys, heat treatment capacity, low density, and processing flexibility.
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Reinforcement.
When nano-TiO2 material reinforced with metal matrix composites, has the potential to produce materials suitable for high temperature applications because of its high thermal conductivity, outstanding mechanical properties plus attractive damping properties. TiO2 is extensively used as a reinforcing phase because it can enhance the hardness, tensile strength and wear resistance of aluminium composites [8–9].
Titanium dioxide or Titania (TiO2) occurs in many crystalline forms, the utmost significant being Anatase and Rutile. Unadulterated titanium dioxide will not exist in nature but comes after Ilmenite or Leuxocene ore. Besides it is easy to exploit from one of the purest forms, rutile beaches. Most of the Anatase form of titanium dioxide is produced in the form of a white powder and the different qualities of Rutile are usually off-white and may even have a slight color reliant on the physical form that disturbs the reflection of the light. Alumina and silica are used as coating material for Titanium dioxide to increase the technical performance. Rutile can be a thermodynamically stable form of titanium dioxide, Anatase will rapidly converted to Rutile at temperatures above 700° C and Rutile melts between 1830 and 1850° C [10].
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A Review on Metal Matrix Nano Particulate Composites.
Zapata [11] showed that the manufacturing of nanocomposites can be divided in to three types, namely "solution mixing, the liquefied state and in-situ polymerization". He also showed that the latex consisted in employing the monomer plus the reagent used amongst the clays. During the polymerization process, the spacing between the layers of clay gradually increased and the dispersion state of the clay increased from intercalated to exfoliate. Benefits of this technique includes i) single-phase casting of the metallocene polymer nanocomposite, ii) enhanced compatibility of the clay with the polymer matrix, iii) the improvement of the dispersibility of the clay.
Zhang Z et al [12] demonstrated in their study that the Orowan equation disclosed that nano-size reinforcement was very beneficial for tribological applications compared to macroscopic size reinforcement. Merely a slight amount of nano-sized reinforcing material is sufficient to provide the base alloy superior wear resistance.
Ray et al [13] have shown that due to the presence of particles at the bottommost portion, a high stirring speed is essential to lift the particles for dispersion, the stirring speed being greater than the speed agitation required to dispense the added particles from above. The benefit of removing the trapped air formed around the particles during the infiltration process is that the porosity of the cast composite is minimized, which can be compensated for the necessity of a high stirring speed, causing a bubble inhalation rate higher in the vortex, causing more porosity in the synthesized composites.
K. R. Padmavathi et al [14] compared the properties of nano and micron sized SiC reinforced with Al6061 with wt. % of 5, 10 & 15 for micron sized SiC and 0.5, 1 & 1.5 for nano sized SiC by stir casting methods. The findings indicate that produced nano composites outperformed micron-sized composites in terms of hardness and wear resistance. Considering every factor shown that nano-sized SiC reinforcement added to an aluminum-based composite at a weight-based ratio of 1.0% had superior wear resistance characteristics compared to micron-sized SiC reinforcement added to an aluminum-based metal matrix composite. In comparison to Al6061-micron sized SiC metal matrix composites, Al6061-nano SiC exhibits lower wear rates and friction coefficients. Comparing wear rates of Al6061-10% micro SiC and Al6061-1.0% nano SiC composites to those of other reinforcing weight percentages, these composites have a low wear rate. Al6061-nano SiC composites have harder values than Al6061-micron SiC composites; the VHN values for micron-sized SiC and nano-sized SiC particles, respectively, are 55, 57, and 59.
Iman S. El-Mahallawi et al [15] studied the microstructure of a cast aluminium alloy by accumulating nanoparticles of Al2O3, TiO2 and ZrO2 of 40 nm particle size to A356 aluminium by stir casting methods. Nano powders are stirred in an A356 matrix at variable speeds of 270, 800, 1500, 2150 rpm at 600° and 700°C which means at both semi-solid and liquid state, with 0–5% by weight, with a stirring time of one minute. The microstructure of the alloy comprises a primary aluminium matrix and an Al-Ti eutectic. The microstructure of as cast displays an even distribution particles in the phases. In the base part of the matrix, the microstructure is dendritic, while in other rheological samples, the main dendritic structure is broken by mechanical stirring. But with continuous agitation, the plastic deformation in the fragmented grains will be substantially reduced. The UTS were 155, 158, 164, 185 and 163 MPa, respectively, with respective elongations of 57%, 64%, 72%, 77% and 49% for 0,1,2,3 and 4 wt. % respectively. The results show, when the weight percentage of TiO2 nanoparticles increased to 3%, the UTS also increased to 185 MPa. Above this % by weight, the UTS decreases as the weight % of TiO2 nanoparticles increases. The ductility reached its maximum for 3% by weight of TiO2 nanoparticles, and then reduced for 4% by weight of TiO2 nanoparticles. Since the hard nature of the TiO2 nanoparticles results in an increase in the position of the local stress concentration, there is an embrittlement effect. These TiO2 particles will restrict the passage of dispersion by creating a stress field in the matrix or causing large differences in elastic behavior between the matrix and the dispersion. Since the intercalated nano TiO2 particles do not react with the matrix, it can be expected that the embrittlement effect of TiO2 is mechanical in nature.
By adopting bottom pouring stir casting technique by in-situ method, H M Nanjundaswamy et al. [16] demonstrated the impact of forged and unforged magnesium-based composites and demonstrated how the BHN and Tensile characteristics will differ in the forged and unforged composites. Due to reduced porosity and intermetallic particle, the BHN and Tensile values for the forged composites were higher than those for the unforged composites.
Amal E. et al. [17] investigated the mechanical performance of pure aluminium reinforced with nano titanium di-oxide particle composites that had a volume percentage of 0.5, 1.5, 2.5, 3.5, and 4.5 and an average diameter of 50 nm. 52, 65, 71, 76, 81, and 85 BHN are the corresponding BHN values. This might be owing to the presence of nanoparticles, which delayed the movement of matrix disruption which may be the principal reasons for improved strength and hardness and due to (a) the existence of relatively harder ceramic particles in the matrix, (b) higher restriction in the localized matrix distortion through the indentation due to their existence, and (c) reduced grain size to nanometer.
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S. Krishnaraj et al [18] studied the hardness behaviour of TiO2-SiC reinforced metal matrix composites made thru powder metallurgy method. The test specimens of metal matrix composites were prepared by varying reinforcement ratio as 5%, 10%, 15% and 20% correspondingly. The BHN values observed were recorded as 15, 26, 30 and 35 respectively, the hardness of the specimen varies because of adding silicon carbide and titanium di oxide to the matrix material. The addition of 10 Percentage of Titanium di-Oxide also has the higher hardness value compared with 10 percentage addition of Silicon Carbide particles.
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Ganesh raja et al [19] synthesized and compared the properties of composites which is produced by stir casting method via Aluminium as base Matrix, TiO2 and SiC as reinforcements in the wt. % of 5 & 10. For TiO2 Particulate composites the UTS observed were 153 & 182 Mpa, the YS were 142 & 149 Mpa respectively and for SiC Particulates composites UTS are 145 and 171 Mpa and YS are 117 and 123 Mpa. He reported that the YS and UTS of TiO2 Particulate composites were greater than that of reinforced with SiC Particulate composite for the same wt. % mainly because of grain refinement in the matrix.
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M. Karbalaei Akbari et al [20] observed changes in weight loss and wear rate, in nano particulate composites. The resistance to wear of the composite is greater than that of the unreinforced alloy. The existence of ceramic nanoparticles protects the matrix and the TiO2 phase from the direct experience of the applied loads. In addition, as the nanoparticles are on the surface, this will lighten the partial shear stress accumulated to get relieved. The outcomes of the wear test exhibited that a substantial development in the wear resistance of the sample was eminent at 1.5 volume % of nanoparticles. An additional rise of nano particle content shows a decrease in wear resistance may be due to clustering phenomena. The laminate layer is clearly visible on the worn surface, which seems to protect the TiO2 surface from direct contact with the abrasive during the wear of these hard ceramic nanoparticles on the matrix interface and TiO2 particle.
Vinaykumar S Shet et al [21] showed that as TiO2 content increases in Al 6063 a marginal improvement of about 6.25%, 18.75%, 37.5%, 43.75, in wear resistance is observed in composites of Al6063 with 2, 4, 6 and 8% wt. and compared with Al-6063 matrix alloy. Absence of porosity in composite material will increases the contact between the sliding surfaces which may limit the surface harshness, along these lines it limits the contact weight and diminishes the chances of molecule separation during sliding. The impact connected to typical load on the wear rate of Al-6063 combination and the composites under sliding speed of 0.3141m/s is delineated. It is seen that with increment in typical load there is increment in wear rate of both the Al-6063 and Al-6063-TiO2 composites. Wear rate can be increments with the expansion in stack in both Al6063 amalgam and Al6063-TiO2 composites which can be credited to higher degree of plastic disfigurement.
The wear behaviour of an Al-2Mg alloy spray produced and the wear behaviour of Al-2Mg-11TiO2 composites made by stir casting were compared by S K Chaudhury [22] and his colleagues. Due to the sample's adhesion characteristics to the sliding disc, which has a high coefficient of friction value at the beginning phases of wear, a higher wear rate is observed at the initial stage. The wear rate of the composite as a function of load shows that it is significantly lower than that of the matrix alloy (spraying and stirring), suggesting that the presence of a harder phase (in this case, TiO2 particles) will result in a lower wear rate. Additionally, under identical test conditions, the wear rate of the spray-formed composite under various loads was lower than that of the stir-cast composite. This difference can be attributed to the lack of a uniform distribution of TiO2 in the matrix phases, which leads to high porosity and inadequate interfacial bonding.
Ganesh Khandoori [23] and his collaborators have studied the wear behaviour of aluminium with TiO2 reinforcement in the ratios of 5%, 10% and 15%, processed by stir casting. The test clearly shows that as the load value increases, the mass loss of all three samples increases, but the rate is different. It is clear that as the TiO2 composition increases, the loss of mass decreases which convey that the mass loss of the composite decreases as the percentage of TiO2 increases. The relationship between the volumetric wear rate and the applied load at a constant sliding speed (2.0106 m/s) shows that the volumetric wear has a lower value for greater percentages by weight of TiO2 particles. The porosity causes a temporary increase in the composite's specific wear rate. Due to the relatively moderate effect on porosity, the wear rate of in situ cast composites with strong reinforcing particles increases slightly as the volume percentage of porosity increases. The link between the mass loss and the sliding distance between the constant load (25 N) and the sliding speed is stronger as the sliding distance rises.
1.7 Problem Formulation
Incorporating nano ceramic, intermetallic, or metallic particle reinforcement into a ductile matrix has produced a promising class of materials known as Nano Particulate Metal Matrix Composites (NPMMCs), according to a critical evaluation of the available literature. Aluminium based NMMC’s can be used for lightweight structural and functional components for automotive and aerospace applications to further decrease cost of transportation, environmental pollution by lowering fuel consumption. Aluminium based MMNCs provide better tribological performances, better castability and dimensional stability, and superior machinability compared with aluminium alloys and aluminium based MMCs with micron sized particles (M Karbalaei Akbari et al [20]).
However, Nano TiO2 particles increases ductility of aluminium matrix composites compared with the same wt. % of micron sized particulate composites. In recent years, the nano-particles of B4C, SiC and Al2O3 have also received attention as particle reinforcement for Aluminium based composites. The present study explores the possibility of reinforcing various nano particles with the sizes of 200nm, 60nm, 25nm and 15nm of TiO2 with LM0 aluminium alloy by using bottom pouring stir casting furnace, which possess outstanding features as mentioned in the following paragraphs.
Stir casting, a method of synthesising metal matrix composites (MMNCs), is less expensive for mass production than other manufacturing processes for generating particle-reinforced aluminum-based MMNCs (Ray [13]), hence it has received a lot of attention. Additionally, using traditional foundry procedures, composites made of aluminium may be manufactured into nearly-net shapes.
The industry and scientific community are paying more attention to aluminum-based nano composites and its alloys as there is a growing need for lightweight materials in automotive and aerospace applications (Ambreen Lateef [24], Charles Chikwendu Okpala [25], and Reddy BS [3]). Typical examples of the components made out of aluminium and its alloys for automotive application include piston, fuel injection pipe, cylinder head, suspension arms and steering systems, car doors etc., (M. Azeem Dafedar [26]).
If the size of the particle decreases the mechanical properties will also vary for the same volume or weight percent of reinforcement (K. R. Padmavathi [14]). So by considering the different factors, the choice of reinforcement in our current investigation has been narrowed down to nano TiO2 with particle size of 200nm, 60nm, 25nm and 15nm with Rutile grade, and 5 wt. % of magnesium is added in order to improve the wettability of the composites which are expected to remain stable in aluminium alloy matrix at elevated service temperatures. The reinforcement phases are expected to serve the interest of automobile industries in the contest of their need for new materials to be employed in various structural and tribological applications.
By varying the particles size the mechanical properties can be varied. Hall-Petch theory states that by reducing the particle size it is seen that the strength as well the ductility properties will also enhances (Sanaty-Zadeh [27], Luo P [28]). M. S. Islam [31] showed that the mechanical properties will increase with decrease of particle sizes until 10 nm. The decrease in 5 nm system was attributed to poor dispersions of nano-particles in the composites which results in decreased properties because of stress concentration effect of agglomerated particles.
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OBJECTIVE OF THE PRESENT WORK.
In the present work an attempt has been made to Prepare, Characterize, Evaluation of Mechanical Properties and Tribological Behavior of LM0 alloy reinforced with various Nano Particle size of TiO2 particulates by stir casting route. Some of the specific objectives are:
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Preparation of LM0 with 200nm, 60nm, 25nm and 15nm TiO2 nano particulate composites to know the effect of reinforcements in steps of 0, 4, 8 and 12 wt. % by using bottom pouring casting furnace.
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Microstructural characterization of prepared composites by using Scanning Electron Microscope, Energy Dispersive Spectroscope and X-Ray Diffractometer to know the uniform distribution of nano TiO2 particles in the LM0 alloy matrix and to know the presence of Titanium and Magnesium in the various sized nano TiO2 particulate composites.
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Further, prepared samples are tested for mechanical properties like hardness, ultimate tensile strength, yield strength and percentage elongation as per ASTM standards of various nano sized TiO2 particulate composites.
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Studies on wear behaviour of various Nano sized TiO2 particulates reinforced LM0 alloy by considering varying parameters like applied load and sliding velocity by keeping sliding distance constant at room temperature by using pin-on-disc wear testing machine.