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Fly ash is a lightweight coal combustion by-product (CCB) separated from the exhaust gases of power generating plants using suspension-fired furnaces in which pulverized coal is used as the fuel. Its physical and chemical properties make it useful in construction and industrial materials, especially in cement manufacturing, concrete, liquid waste stabilization, and hydraulic mine backfill. The addition of fly ash into aluminum alloys has the potential to reduce the cost and density of aluminum castings while improving other physical and mechanical properties of the resulting metal matrix composites (MMCs). <p> This study investigated the effect of fly ash addition on the mechanical properties and microstructural behaviour of aluminum casting alloy A535. The unreinforced A535 alloy and its MMCs containing a mixture of 5 wt.% fly ash and 5 wt.% silicon carbide, 10 wt.% fly ash and 15 wt.% fly ash were investigated in the as-cast and solution heat treated conditions. Microhardness measurements, Charpy impact testing, tensile testing, optical microscopy, scanning electron microscopy (SEM), energy dispersive X-ray spectrometry (EDS), inductively coupled plasma/mass spectrometry (ICP/MS), X-ray diffractometry (XRD), and X-ray fluorescence spectroscopy (XRF) were used to evaluate these effects. <p> The results of this study show that increasing the fly ash content of the melt increased the porosity of the castings, which ultimately affected the density, tensile and impact properties of the MMCs. The density, microhardness, tensile strength and Charpy impact energy of the composites decreased with increasing fly ash content. The decline in density of the MMCs was due to extensive porosity developed with fly ash addition. Depletion of solid solution strengthening magnesium in the matrix was the reason observed for the decline in hardness. The loss in Charpy impact energy and tensile properties of the MMCs are also attributed partly to the depletion of solid solution strengthening magnesium atoms from the matrix and partly to porosity. <p> Microstructural studies revealed non-uniform distribution of reinforcement particles in the composites. The fly ash particles were found to congregate at the boundaries of a-aluminium dendrites in the castings. Mg content of A535 alloy decreased with increasing weight fraction of fly ash. Mg was found to be tied up in a complex network of Mg2Si thereby reducing its availability in the matrix for solid solution strengthening.

Fly ash is a lightweight coal combustion by-product (CCB) separated from the exhaust gases of power generating plants using suspension-fired furnaces in which pulverized coal is used as the fuel. Its physical and chemical properties make it useful in construction and industrial materials, especially in cement manufacturing, concrete, liquid waste stabilization, and hydraulic mine backfill. The addition of fly ash into aluminum alloys has the potential to reduce the cost and density of aluminum castings while improving other physical and mechanical properties of the resulting metal matrix composites (MMCs). <p> This study investigated the effect of fly ash addition on the mechanical properties and microstructural behaviour of aluminum casting alloy A535. The unreinforced A535 alloy and its MMCs containing a mixture of 5 wt.% fly ash and 5 wt.% silicon carbide, 10 wt.% fly ash and 15 wt.% fly ash were investigated in the as-cast and solution heat treated conditions. Microhardness measurements, Charpy impact testing, tensile testing, optical microscopy, scanning electron microscopy (SEM), energy dispersive X-ray spectrometry (EDS), inductively coupled plasma/mass spectrometry (ICP/MS), X-ray diffractometry (XRD), and X-ray fluorescence spectroscopy (XRF) were used to evaluate these effects. <p> The results of this study show that increasing the fly ash content of the melt increased the porosity of the castings, which ultimately affected the density, tensile and impact properties of the MMCs. The density, microhardness, tensile strength and Charpy impact energy of the composites decreased with increasing fly ash content. The decline in density of the MMCs was due to extensive porosity developed with fly ash addition. Depletion of solid solution strengthening magnesium in the matrix was the reason observed for the decline in hardness. The loss in Charpy impact energy and tensile properties of the MMCs are also attributed partly to the depletion of solid solution strengthening magnesium atoms from the matrix and partly to porosity. <p> Microstructural studies revealed non-uniform distribution of reinforcement particles in the composites. The fly ash particles were found to congregate at the boundaries of a-aluminium dendrites in the castings. Mg content of A535 alloy decreased with increasing weight fraction of fly ash. Mg was found to be tied up in a complex network of Mg2Si thereby reducing its availability in the matrix for solid solution strengthening.

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Al-Mg alloys were infiltrated into porous alumina preforms at temperatures greater than 950°C where significant amount of nitride forms in the matrix. The present work aims to obtain a process window for growing A1N rich composites over uniform thicknesses so that bulk fabrication of these composites could be carried out. Initial experiments were carried out in a thermo-gravimetric analyser (TGA) to establish suitable conditions for growing useful thicknesses. Al- 2wt% Mg alloy, alumina preforms of particle size 53-63μm and N2 - 2% H2 (5ppm O2) were used for the present study based on previous work carried out in the fabrication of MMCs at low temperatures. Experiments carried out in the TGA indicate that oxygen in the system has to be gettered for the growth of nitride rich composites. Infiltration heights of about 8mm were obtained using an external getter (Al - 5wt%Mg) alloy in addition to the base alloy used for infiltration. The above process conditions were subsequently employed in a tube furnace to fabricate bulk composites and to study the effect of temperature on the volume fraction of aluminium nitride in the matrix. The volume fraction of nitride in the composite varied between 30 and 95 vol % with increase in process temperature from 950°C to 1075°C. Microstructures of these composites indicate that A1N starts to form on the particle surface and tends to grow outwards. The metal supplied through channels adjacent to the particle surface nitride until a point is reached when the composite growing from the adjacent particles meet each other and isolate the melt underneath from nitrogen thereby leading to a metal rich region underneath. Increase in temperature results in an increased nitridation rate resulting in reduced metal pocket size. Composites fabricated at 975°C had a minor leak at the O-rings, which seal the tube. This led to infiltration under conditions of varying oxygen partial pressure leading to different nitride fractions in the composite. The above fact was confirmed by conducting an experiment with commercial purity nitrogen, which has an oxygen content of about 5000ppm. The composite had an A1N content of about 30% whereas the composite fabricated with N2 -2%H2 (5ppm oxygen) showed a nitride content of 64%. This suggests that one can vary the nitride content in the composite by varying the oxygen content in the system at a particular process temperature. The hardness of the matrix increases with increase in process temperature from 3.5 ± 0.7 GPa at 975°C to about 9.8 ± 0.9 GPa at 1075°C. Porosity was observed in the composite processed at 1075°C. This increased porosity leads to decreased hardness though the nitride content in the composite has increased by 11%. The scatter in the data is attributed to variations in the microstructure as well as due to interference from underlying metal pockets or particles as well as due to porosity introduced in the composite at high processing temperatures.

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Metal matrix composites (MMCs) are emerging as advanced engineering materials for application in aerospace, defence, automotive and consumer industries (sports goods etc.). In MMCs, a metallic base material is reinforced with ceramic fiber, whisker or particulate in order to achieve a combination of properties not attainable by either constituent individually. Aluminium or its alloy is favoured as metallic matrix material because of its low density, easy fabricability and good engineering properties. In general, the benefits of aluminium metal matrix composites (AMCs) over unreinforced aluminium alloy are increased specific stiffness, improved wear resistance and decreased coefficient of thermal expansion. The conventional reinforcement materials for AMCs are SiC and AI2O3. In the present work, boron carbide (B4C) particles of average size 40μm were chosen as reinforcement because of its higher hardness (very close to diamond) than the conventional reinforcement like SiC, AI2O3 etc. and of its density (2.52 g cm"3) very close to Al alloy matrix. In addition, due to high neutron capture cross-section of 10B isotope, composites containing B4C particle reinforcement have the potential for use in nuclear reactors as neutron shielding and control rod material. Al-5%Mg alloy was chosen as matrix alloy to utilize the beneficial role of Mg in improving wettability between B4C particles and the alloy melt. (Al-5%Mg)-B4C composites containing 10 and 20 vol% B4C particles were fabricated. For the purpose of inter-comparison, unreinforced Al-5%Mg alloy was also prepared and characterized. The Stir Cast technique, commonly utilized for preparation of Al-SiC, was adapted in this investigation.The Composites thus prepared was subsequently hot extruded with the objective of homogenization and healing minor casting defects. Finally the unreinforced alloy and its composites were characterized in terms of their microstructure, mechanical and thermo-physical properties, sliding wear behaviour and neutron absorption characteristics. The microstructures of the composites were evaluated by both optical microscope and scanning electron microscope (SEM). The micrographs revealed a relatively uniform distribution of B4C particles and good interfacial integrity between matrix and B4C particles. The hot hardness in the range of 25°C to 500°C and indentation creep data in the range of 300°C to 400°C show that hot hardness and creep resistance of Al-Mg alloy is enhanced by the presence of B4C particles. Measurement of coefficient of thermal expansion (CTE) of composites and unreinforced alloy upto 450°C showed that CTE values decrease with increase in volume fraction of reinforcement. Compression tests at strain rates, 0.1, 10 and 100 s-1 in the temperature range 25 - 450 °C showed that the flow stress values of composites were, in general, greater than those of unreinforced alloy at all strain rates. These tests also depicted that the compressive strength increases with increase in volume fraction of reinforcements. True stress values of composites and unreinforced alloy has been found to be a strong function of temperature and strain rate. The kinetic analysis of elevated temperature plasticity of composites revealed higher stress exponent values compared to unreinforced alloy. Similarly, apparent activation energy values for hot deformation of composites were found to be higher than that of self-diffusion in Al-Mg alloy. Tensile test data revealed that the modulus and 0.2% proof stress of composites increase with increase in volume fraction of the reinforcements. Composites containing 10%BUC showed higher ultimate tensile strength values (UTS) compared to unreinforced alloy. However, composites with 20%B4C showed lower UTS compared to that of the unreinforced alloy. This could be attributed to increased level of stress concentration and high level of plastic constraint imposed by the reinforcing jparticles or due to the presence solidification-induced defects (pores and B4C agglomerates ). Sliding wear characteristics were evaluated at a speed of 1 m/s and at loads ranging from 0.5 to 3.5kg using a pin-on-disc set up. Results show that wear resistance of Al-5%Mg increases with the addition of B4C particles. Significant improvement in wear resistance of Al-5%Mg is achieved with the addition of 20% B4C particles. SEM examination of worn surfaces showed no pull-out of reinforcing particles even at the highest load of 3.5 kg, thus confirming good interfacial bonding between dispersed B4C particles and Al alloy matrix. The neutron radiography data proved that (Al-5%Mg)-B4C composites possess good neutron absorbing characteristics. From the experimental data evaluated in the "study, it may be concluded that (Al-5%Mg)-B4C composites could be a candidate material for neutron shielding and control rod application. The enhanced elevated temperature-strength and favourable neutron absorption characteristics of these composites are strong points in favour of this material.

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