O objetivo deste trabalho foi de otimizar o processo de fabricação da placa reforçadora de solo, fabricada pelo processo de injeção sob baixa pressão em liga de alumínio. Atualmente, a liga utilizada no processo é a SAE 305 (AA 413) e problemas de falha do componente em campo tem sido reportados pelos clientes. As peças estudadas referem-se às placas acessórias utilizadas para fornecer sustentação durante a entrada e saída de vaus por carros de combate do Exército Brasileiro, anteriormente adquiridas no mercado internacional e agora produzidas internamente. O estudo focou na alteração da composição química da liga, baseado na liga de alumínio da peça importada, tratamento de banho com modificação do silício, refino de grão e modificação no projeto do molde permanente. Adquiriu-se junto ao fornecedor a liga de Al9Si0,3Mg visando a fabricação das peças com tratamento térmico T6. Para obtenção das propriedades mecânicas foram realizados ensaios de tração, dureza Brinell e impacto. Para caracterização metalúrgica foram realizados ensaios metalográficos com auxílio de microscopia óptica. Verificou-se que a presença de magnésio na liga Al-Si exclusivamente com tratamento térmico T6, alterou o comportamento mecânico da peça melhorando seus resultados. O tratamento de banho com modificador de silício a base de sódio não produziu resultados significativos. Finalmente, realizou-se simulação do preenchimento da molde via software CAE Click2Cast, modo injeção de baixa pressão, para caracterização dos defeitos e sugestões de melhoria no sistema de alimentação. Deste trabalho, conclui-se que as melhores propriedades mecânicas de resistência a tração e dureza foram obtidas com a alteração da liga SAE 305 para a liga Al9Si0,3Mg com tratamento térmico T6 e que para atingir melhores resultados deve-se introduzir ao processo um novo molde permanente com refrigeração e alimentação adequada da peça. / The objective of this research was to optimize the manufacturing process of the reinforcing plate of soil, manufactured by the injection process under low pressure in Al-Si alloy. Currently, the alloy used in the process is SAE 305 (AA 413) and mechanical resistance problems, when used in the field, have been reported by customers. Currently, the alloy used in the process is SAE 305 (AA 413) and field component failure problems have been reported by customers. The studied pieces refer to the accessory plates used to provide support during the entry and exit of vats by tanks of the Brazilian Army, previously acquired in the international market and now produced internally. The study focused on the alteration of the chemical composition of the alloy, based on the aluminum alloy of the imported part, bath treatment with silicon modification, grain refining and modification in the permanent mold design. The Al9Si0.3Mg alloy was purchased from the supplier to manufacture the T6 heat treated parts. To obtain the mechanical properties tensile tests, Brinell hardness and impact were performed. For metallurgical characterization, metallographic tests were performed with the aid of light microscopy. It was verified that the presence of magnesium in the Al-Si alloy exclusively with T6 heat treatment, altered the mechanical behavior of the part improving its results. Bath treatment with sodium silicon modifier did not produce significant results. Finally, the mold filling simulation was carried out using CAE Click2Cast software, low pressure injection mode, to characterize the defects and suggestions for improvement in the feed system. From this work, it was concluded that the best mechanical properties of tensile strength and hardness were obtained with the change of the SAE 305 alloy to the Al9Si0.3Mg alloy with T6 thermal treatment and that to achieve better results a new permanent mold with cooling and proper feeding of the part.

L’objectif de ce travail est d’établir des relations entre chimie d’interface et propriétés mécaniques dans les assemblages bimétalliques. Il met en évidence que les mécanismes qui contrôlent le développement d’une interface entre alliage Al-Si et renfort ferreux ou titane ont une influence majeure sur les propriétés mécaniques de cette interface. La caractérisation mécanique des interfaces est réalisée par un test de flexion 4 points sur des lames bimétallique élaborées par aluminiage au trempé sur lesquelles un raidisseur est rapporté par collage ou surmoulage. L’évolution de la chimie de la zone de réaction interfaciale est provoquée par un traitement thermique à 535°C à différents temps. La caractérisation des zones de réaction ainsi que des chemins de fissuration est réalisée par diffraction des rayons X et microsonde électronique. Pour les interfaces Fe/A-S7G03 brutes d’élaboration, avant traitement thermique, l’analyse des essais mécaniques conduit à l’obtention d’une valeur du taux de restitution d’énergie de 23 J/m2 qui correspond à la propagation d’une fissure dans la phase η−Al5Fe2(Si). En ce qui concerne les interfaces Ti/A-S7G03, leur force n’a pas permis la propagation d’une fissure dans les conditions de l’essai. A la suite d’un traitement thermique à 535°C, les interfaces Fe/A-S7G03 sont fragilisées par le mécanisme de croissance de la couche de réaction interfaciale qui conduit à l’apparition de porosités Kirkendall en son sein. A l’inverse, dans le cas des interfaces Ti/A-S7G03, aucun affaiblissement de l’interface n’est associé au traitement thermique en raison d’un mécanisme de croissance différent. / The objective of this work is to establish the relationships between interface chemistry and mechanical properties in bimetallic assemblies. It proves that the mechanisms which control the development of an interface between Al-Si alloy and titanium or ferrous reinforcement have a major influence on the mechanical properties of this interface. The mechanical characterization of these interfaces is performed by a 4-point bending test on the bimetallic plates elaborated by hot dip aluminizing on which a stiffener is joined by bonding or overmolding. The chemistry evolution of the interfacial reaction zone is induced by a heat treatment at 535 °C at different reaction times. The characterization of reaction zones and the crack paths is performed by X-ray diffraction and electron probe microanalysis. Before heat treatment, the analysis of mechanical tests performed on Fe/A-S7G03 interfaces leads to a value for the energy release rate of 23 J/m2 which corresponds to a crack propagation in the η- Al5Fe2 (Si) phase. As regards the Ti/A-S7G03 interfaces, their strength did not allow a crack propagation under the test conditions. After a heat treatment at 535°C, the Fe/A-S7G03 interfaces are weakened by the growth mechanism of interfacial reaction layer which leads to the appearance of Kirkendall voids within it. Conversely, in the case of Ti/A-S7G03 interfaces, the heat treatment is not associated with any weakening of the interfacial zone because of a different growth mechanism.

Aluminium silicon alloy has been found to be advantageous in many automobile components like pistons, cylinders, brakes and clutches. The main objective in using these alloys is to obtain lightweight and low friction at a reasonable cost without sacrificing reliability and durability. Out of all the tribological components piston skirts, piston rings and cylinder liners, have to face the most hostile of environments in an internal combustion engine. Wear mechanism of these components have been identified as abrasion, scuffing and corrosion. Narrowing down the line of interest, cylinder wear is more important than ring wear to both the engine manufacturer and the user, as cylinders are more expensive to replace than piston rings. Wear of piston ring and cylinder combination have been studied using a wide range of techniques. It is difficult to predict the tribological performance of these parts in an engine, even with the most well designed laboratory tests, due to chemical, thermal and mechanical complexities in the operating environment. Therefore, a good correlation is sought from the wear behaviour of test bed engines and laboratory tests. This should form the basis of further development particularly in terms of efficiency, weight eduction and wear life improvement of the components. Many ASTM bench-wear tests are used to study wear, some of the common tests being ball-on-disc and pin-on-disc testing. From these tests, a large database of wear information can be achieved and they offer rapid and low cost means of comparison. The only drawback is that the real components are not tested. However, since the bench tests can never simulate the engine environment completely, engine tests are always required for final verification. This thesis work reports preliminary studies of machining damage and wear in actual engine bore to set a bench mark, followed by a set of unidirectional sliding bench tests to study the wear of aluminium alloy under lubricated conditions, to classify the different wear regimes in boundary lubrication zone under different pressure conditions, and to study the effect of a surface modification technique, etching, which improves wear properties. The investigation is divided into four parts. 1. Study of subsurface damage in an actual cylinder surface as introduced by prior machining and actual worn case: A study of the microstructure of bores, processed through a range of machining variables; feed and speed, are investigated in this part of the thesis. This work suggests that the first step of rough machining may be responsible for the microstructure of the finished bore even though subsequent processing steps are intended to remove all prior damages. This also includes some observations of worn surface of an actually run engine, locating the various worn spots and studying the cause of this damage 2. Bench wear test in pin-on-disc under dry and lubricated condition with varying load and lubricant: After setting a benchmark on wear in engine using actual worn cylinder bore, a set of bench tests were carried out on aluminium alloy. Here, steel pins are slid on aluminium silicon alloy discs in the boundary lubrication regime in the presence of one drop of oil. The effect of pure hexadecane and engine oil containing additives on friction and wear are analysed and the data are discussed in terms of the formation of a mechanically mixed layer at the interface. 3. Ultra-mild Wear in Lubricated Tribology of an Aluminium Alloy: To study the different wear regimes in boundary lubrication zone, flat faces of cylindrical steel pins were slid on an eutectic aluminium silicon alloy under lubricated condition in the 1-100 MPa mean contact pressure range and 0.2 m/s sliding speed. Two transitions in wear rate were observed, at 10 MPa and 70 MPa. The wear rate in the 1-10 MPa regime was found to be very small and within the measuring instrument resolution and also insensitive to contact pressure. The regime is designated ultra-mild wear. Lack of plastic flow, minimal fragmentation of silicon particles and the presence of undistorted voids on the fractured and unfractured silicon particles in the subsurface suggest that the state of stress in the near surface region is elastic. Contact mechanical calculations demonstrate that at contact pressures less that 13.7 MPa the system is likely to shakedown to an elastic state. 4.Ball-on-disc wear tests for etched and unetched samples: In the fourth part of the thesis, comparative studies have been done between the as polished and chemically treated samples. Formation of grooves in a ball-on-disc experiment is observed on etched and unetched flats as a function of normal load and sliding distance. The groove is initially formed by plastic flow, and then expanded by micro-abrasion as the ball continues to slide on the groove. However etching causes surface hardening of the alloy, but, more importantly, creates a surface topology that reduces the peak contact pressure, which inhibits further plastic flow in the subsurface.

Magnesium alloys have emerged as a promising material for light-weighting due to their potential for higher weight saving compared with advanced high-strength steel, aluminium alloys and glass fibre reinforced polymer composites based on equal stiffness or strength. Even though magnesium alloys offer low density, high strength to weight ratio and excellent machinability their poor creep resistance and low yield strength at elevated temperatures (~150oC) restricts their use in automotive powertrain applications. Possible ways of improving the creep resistance include development of creep resistant alloys and/or reinforcing the alloy with ceramic particulates, fibres/whiskers. Several magnesium alloys such as – Mg-Zr based alloys, Mg-Al-RE alloys (RE: rare earth), Mg-Al-Ca alloys, Mg-Al-Sr alloys, Mg-Al-Sr-Ca alloys, Mg-Al-Si alloys offer improvement in creep resistance to different extent. However, these alloys are relatively expensive than the widely used Mg-Al-Zn alloys. Some of these alloys are unsuitable for die casting application due to cracking or die filling problems for example, in Ca and Sr containing alloys their content must be controlled to avoid castability problems. Discontinuous reinforcement of magnesium alloys opens up wide variety of casting techniques for production. Most of the components do not require high performance capability all throughout the component. Squeeze casting technique can be used to economically produce selectively reinforced composites having complex near-net-shape components. By selectively reinforcing only the regions of stress concentration, material property can be optimised at the same time lowering both the cost of manufacturing and machining. In the present study, wear behaviour of Saffil short fibre reinforced AZ91D Mg alloy composite prepared by squeeze casting is explored. The Mg-Saffil composite had a two dimensional planar random fibre orientation which was inherent to the fabrication process of porous fibre preform. In the as-polished specimen fibres protrude out of the Mg matrix due to differential polishing. The Mg-Saffil composites were subject to unidirectional sliding wear against steel counterface under nominally dry condition in ambient atmosphere at low velocities, to simulate the piston reversal at the top dead centre of an engine wherein lubrication starvation results in wear of engine cylinder. The fibres protruding out of the magnesium matrix prevent the softer Mg matrix coming in contact with the counterface material. The worn surface was examined by means of scanning electron microscopy and the physical and chemical changes caused by the wear processes were characterised using different spectroscopic techniques. The effect of fibre distribution and fibre orientation on wear of the composite was studied. Depending on the radius of curvature of the counterface, inhomogeneities in the fibre distribution up to a certain length scale were permissible without deteriorating the wear resistance of the composite. The normal fibre orientation proved deleterious to the wear of the counterface. But wear of the composite was independent of the fibre orientation of the wear surface. In contrast to unreinforced AZ91 Mg alloy which undergoes extensive wear, the steel counterface was machined by the hard alumina fibres protruding out of the matrix. With progressive sliding a discontinuous patch of transferred material formed on the worn surface. Eventually, an oxidised iron-rich transfer layer formed on the worn surface due to compaction of the transferred material and wear debris under the combined action of applied normal load and frictional force. The coefficient of friction plateaus following an initial rapid increase with the increase in the areal coverage of the transfer layer. The abrupt increase in friction coincides with the change in contact at the sliding interface from protruding alumina fibres/steel counterface to mostly between the transferred layer and steel counterface. The increase in friction due to the iron-rich transfer layer formed on the worn surface induced bending stresses in the fibre. A correlation between the incipient fibre fracture and build-up of the transfer layer was observed. Wear of the composite was governed by the dawn of the fibre fracture event, which in turn leads to three-body wear. Diamond-like carbon coatings are well-known for their low friction, high hardness and elastic modulus, chemical inertness and optical transparency. They have found widespread use due to their superior tribological characteristics as protective coatings for magnetic storage media (hard-disk drives), in micro-electromechanical devices (MEMS), biomedical applications (joint implants, artificial heart valves), optical windows (anti-reflection coating) and razor blades. The physical and mechanical properties of these coatings can be tailored by controlling the sp3 /sp2 ratio and modification via alloying with metals such as W, Ti, Cr, Al; or non-metallic elements such as B, N, F, Si. A tungsten doped hydrogenated diamond-like carbon coated steel counterface was used to rule out or minimise any chemical and physical interaction between the composite and the counterface. The composite exhibited a higher wear resistance when slid against a DLC coated steel counterface due to ease of interfacial sliding between the carbon-rich transfer layer and the DLC coated counterface. The transition from ultra-mild to mild wear was not altogether suppressed but delayed to higher loads, prolonging the ultra-mild wear regime. As a result of reduced friction the point of maximum shear stress recedes from the surface, which manifests as subsurface cracks. The dominant wear mechanism of Mg-Saffil composite sliding against the DLC coated counterface was delamination wear.

Un protocole expérimental a été développé dans cette thèse pour étudier l'influence de la microstructure héritée du procédé de fonderie dit Procédé à Modèle Perdu sur le comportement en fatigue oligocyclique des alliages Al-Si à température ambiante. Dans un premier temps, la microstructure des alliages étudiés a été caractérisée à la fois en 2D et en 3D. Les éprouvettes les plus appropriées et les plus représentatives et les régions d’intérêt où le suivi in-situ est réalisé (ROIs) ont été sélectionnées par une caractérisation préliminaire en tomographie aux rayons X. Cette caractérisation 3D est également nécessaire pour comprendre les mécanismes d’endommagement après rupture de l’éprouvette. Les observations in-situ réalisées en surface en utilisant un microscope longue distance (Questar) et en volume avec la tomographie aux rayons X permettent de suivre l’amorçage et la propagation des fissures et ainsi d'identifier la relation entre les mécanismes d’endommagement et les microstructures moulées. Les champs de déplacement et de déformation en 2D/3D mesurés à l'aide de la Corrélation d'Images Numériques et la Corrélation d’Images Volumiques permettent d'analyser la relation entre les champs mesurés et les mécanismes d'endommagement. L'analyse post-mortem et la simulation éléments finis ont permis de compléter l’analyse des mécanismes d’endommagement. Les grands pores favorisent l'amorçage de fissures car ils augmentent fortement le niveau de contrainte locale. Les inclusions dures (phase Si, intermétalliques au fer et phases au cuivre) jouent un rôle important dans l’amorçage et la propagation des fissures en raison des localisations de déformation sur ces inclusions / An experimental protocol was developed in this thesis in order to study the influence of casting microstructure on the fatigue behavior in Lost Foam Casting Al-Si alloys in tension and in Low Cycle Fatigue at room temperature. First of all, the microstructures of studied alloys were thoroughly characterized both in 2D and in 3D. The most suitable and representative specimens and Region of Interest (ROIs) where the in-situ monitoring was performed were selected through a preliminary characterization using X-ray tomography, which is also necessary to understand damage mechanisms after failure. In-situ observations performed on surface using Questar long distance microscope and in volume using X-ray tomography allow following cracks initiations and their propagations and thus allow identifying the relation between damage mechanisms and casting microstructure. 2D/3D displacement and strain fields measured using Digital Image Correlation and Digital Volume Correlation allows analyzing the relation between measured fields and damage mechanisms. Postmortem analysis and FEM simulation gave more information for the damage mechanisms. Large pores favor crack initiation as they strongly increase local stress level. Hard inclusions (Si phase, iron intermetallics and copper containing phases) also play an important role in crack initiation and propagation due to strain localizations at these inclusions

The compression behavior of a newly developed near eutectic Al-Si based cast alloy with three different microstructures has been investigated in the present work. Microstructures with modified and unmodified Si particles and matrix with different tempers are investigated. The main objective of this work is to understand the effect of heat treatment and modification on the fracture behavior of the alloy under compression. This alloy is subjected to compressive loading at different strain rates and temperatures during the operation of the engines. Hence, the effect of strain rates and temperatures is also considered. The compression tests are carried out at different strain rates from quasi-static to dynamic viz., 3*10-4 to 102/s and three different temperatures RT, 100°C and 200°C. Microstructure of the alloys studied predominantly consists of eutectic colonies of α-Al and Si with a few interspersed α-Al dendrites. Modified alloy has more globular Si particles than unmodified alloy. Heat treated alloys are found to have hardening precipitates S’ & Al7Cu4Ni and 3-7 atomic layer thick zones, which may be precursors to S’ phase. A variety of large intermetallics, viz., plate like particles Al4.5FeSi, Chinese script like particles Al19Fe4MnSi2 and bulky phase Al3NiCu are also observed in the alloys. Mechanical behavior of the alloys is found to be different for different microstructures. Modification improves strength and ductility. Heat treatment improves strength of the alloy at the expense of ductility. A transition in mechanical behavior is observed after a particular strain rate for all the alloys studied. This transition strain rate is dependent on heat treatment, Si particle size and temperature. This transition can be explained on the basis of dislocation-precipitate and dislocation-Si particle interactions. Work hardening behavior of the alloys depends on the matrix microstructure in the unmodified alloys, and both matrix and particles play a role in the modified alloy. A statistically robust quantitative micro structural analysis has been carried out after compressing the samples at various strain rates and temperatures. The unique contribution of this work is the understanding of combined effect of strain rate and temperature on Si particle fracture characteristics in the alloy with different microstructures. From the fracture characteristics of Si particles, it is concluded that both dislocation pile-up mechanism and fibre loading are responsible for particle fracture in the modified alloy, whereas the fibre loading mechanism alone is sufficient to explain the particle fracture characteristics in the unmodified alloy. Si particles in the modified condition are found to cleave along the lowest surface energy planes {112} & {110} and the particles with orientations {112} & {111} are more prone to fracture. In addition to Si particle fracture, elongated Fe rich intermetallic particles are also seen to show peculiar fracture behavior. The Al4.5FeSi intermetallics with (100) as the plane of the plate cleave along (100) planes. This is a novel finding in this work and could have immense implications on the role of Fe impurities in the fracture behavior of these alloys. Moreover, since these cleavage fractures are seen to be more than 200 microns in size (which implies that the real penny shaped crack would be even larger) their role cannot be assumed to be negligible, as was previously thought. The load sharing between the Al matrix and eutectic Si particles are simulated by microstructure based finite element modeling. The program OOF (Object-Oriented Finite element analysis) is used to generate the finite element meshes for real microstructures with different Si morphology. The experimentally obtained stress – strain properties of the alloy is given as an input to describe the plastic behavior of the Al matrix, in the finite element simulation. This analysis helps to understand the effect of particle size, shape, orientation & clustering and matrix temper on the stress transferred to the Si particles. Combination of Electron Back-Scattered Diffraction (EBSD) and frequency shift, polarized micro-Raman technique is applied to validate the stress states in Si particles with {111} orientations. The stress at fracture of Si particles is also estimated from Raman technique. Even though the alloys with different microstructures show different mechanical behavior, the sequence of fracture mechanisms is found to be same for all the alloys. The failure occurs in three stages: cracking of Si particles at low strains, micro-crack formation along the fractured particles, micro-crack coalescence and propagation leading to final failure. Thus, the proposed analysis links various deformation mechanisms ranging from nano precipitate-dislocation interactions to micro short-fiber theory of load sharing by eutectic silicon along with coupled effect of strain rate and temperature. In addition, negative strain rate sensitivity is also observed in the lower strain rate regimes (3*10-4, 10-3& 102/s) at RT and 100°C for all the three alloys, and serrated flow is also observed in the same strain rate and temperature regimes. Some of the features of serrated flow can be explained by the dynamic strain aging model and some other features by precipitate shearing.