Um modelo computacional autoconsistente para a cinética da descarga em um plasma frio, fracamente ionizado, do tipo produzido em tubos de descarga, foi desenvolvido. Ele foi utilizado para investigar a dinâmica das várias propriedades do plasma, tais como temperaturas, densidades e fluxos das espécies que o compõe. Em particular, o modelo desenvolvido considera explicitamente a composição do plasma contendo várias espécies em vários estados de excitação eletrônica. Pode-se determinar a dinâmica das populações envolvidas nas transições laser do átomo de cobre, num modelo autoconsistente para lasers operando em altas taxas de repetição (-5KHz). O modelo mais completo construido considera cinco níveis para o gás tampão (Ne) e nove níveis para o átomo de cobre. O laser de cobre apresenta duas transições, uma no verde e outra no amarelo (5106 A e 5782 A), ambas terminando em estados metaestáveis de longa duração ( -270 J.LS), no átomo livre. No caso mais geral foram considerados trinta processos para determinar a dinâmica do plasma. O tratamento considera, primeiramente, somente a variação temporal e foi utilizado para estudar o plasma formado por três combinações diferentes de espécies: o gás de He puro; a mistura de He:Cu e por último a mistura Ne:Cu, correntemente utillizada em lasers a vapor de cobre. A evolução temporal da temperatura de elétrons, temperatura dos átomos e densidades das espécies, em particular a das espécies excitadas nos niveis de transição laser, pode ser determinada e os resultados comparados com resultados experimentais e de simulação reportados na literatura, mostrando boa concordância no comportamento geral. Verificou-se neste modelo que o principal mecanismo de desexcitação do nível metaestável inferior da transição laser são as colisões superelásticas e não a desativação via interação com as paredes (difusão). Após este primeiro tratamento o modelo passou a considerar também a dependência radial do plasma numa simetria cilíndrica (modelo radial). Neste caso, o efeito de penetração do campo elétrico é explicitamente considerado e o modelo pode ser aplicado tanto a tubos de pequeno como de grande diâmetro, uma vez que o diâmetro é uma grandeza fundamental para a obtenção de lasers de alta potência. Demonstrou-se que esse efeito produz uma distribuição de população dos níveis envolvidos nas duas transições laser (verde e amarela) do cobre, temporalmente distintas e crescentes da borda para o centro, o que concorda com resultados da literatura. Assim, o pulso do laser irá se iniciar com a emissão verde na borda do tubo, conforme predições de nosso modelo. Determinou-se também que existe um limite máximo para o comprimento do tubo do laser, decorrente da existência de uma janela temporal de ganho (-100 ns). / A self-consistent computational model was developed to describe the electrical discharge in a cold plasma, weakly ionized, of the kind usually produced in discharge tubes. The various properties of the species of the plasma as temperature of the electrons, its densities and fluxes could then be obtained. In particular, the model explicitly considers the plasma containing different species in different state of electronic excitation. From these quantities, one can determine the dynamics of the populations involved in the copper atomic laser transition, in a self-consistent model for lasers operation in high repetition rates (-5KHz). The most complete model developed takes into account five level for the buffer gas and nine levels for the copper atom. The copper laser shows two transitions, one in the green and other in the yellow, (5106 Å e 5782 Å), both ending in metaestable states of long duration (~270 µs), in the free atom. In the most complete case studied, thirty processes were considered in the calculations of the plasma dynamics. The formalism first considers solely the temporal dependence and it was used to study the plasma formed by three species: pure He; He and Cu; and Ne and Cu, the last one been currently used in copper vapor lasers. The time dependent populations of the electrons temperature, atoms temperature and densities, in particular the excited levels involved in the laser transitions, could be determined and the results were compared with experimental and simulated results of literature, showing a general good agreement. It was verified, in this model, that the main deexcitation mechanism of the lower metastable laser level is superelastic collisions and not deexcitation via interactions with the walls (diffusion). Therefore, the model was extended to take into account the radial dependence of the plasma in a cylindrical symmetry (radial model). In this case, the skin penetration effect of the electrical field was explicitly considered and the model can then be applied to either small and large diameters, as the diameter is a fundamental parameter for obtaining high power lasers. It is shown that this effect produces a temporally distinct population distribution in the levels of the laser transitions (yellow and green) of the copper atoms, that start in the border and goes to the center, in agreement with the literature. Therefore, the laser pulse starts with the green emission in the border, according to the prediction of our model. It was also found that there is a limit for the maximum length of the laser tube due to the existence of a time window for the positive gain of the laser (~100 ns).

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.

The separation and reattachment of the suction surface boundary layer in a low pressure turbine is characterized using large-eddy simulation at Re=68,000 based on freestream velocity and suction surface length. A high pass filtered Smagorinsky model is used for modeling the sub-grid scales. The onset of time mean separation is at s=so = 0:61 and reattachment at s=so = 0:81, extending over 20% of the suction surface. The boundary layer is convectively unstable with a maximum reverse flow velocity of about 13% of freestream. The breakdown to turbulence occurs over a very short distance of suction surface which is followed by reattachment. Detailed investigations into the structure and kinematics of the bubble and turbulence statistics are presented. The vortex shed from the bubble, convects downstream and interacts with the trailing edge vortices increasing the turbulence intensity. On the suction side, dominant hairpin structures near the transitional and turbulent flow regime are observed. These hairpin vortices are carried by the freestream even downstream of the trailing edge of the blade with a possibility of reaching the next stage. Longitudinal streaks that evolve from the breakdown of hairpin vortices formed near the leading edge are observed on the pressure surface.

This study presents the results of an experimental study that investigates the effects of uniform/waveform tip injection along the camberline on the total pressure loss characteristics downstream of a row of Low Pressure Turbine (LPT) blades. The experiments are performed in a low speed cascade facility. This injection technique involves spanwise jets at the tip that are issued from a series of holes along the camber line normal to the freestream flow direction. The injection mass flow rate from each hole is individually controlled using computer driven solenoid valves and therefore the flow injection geometrical pattern at the tip can be adjusted to any desired waveform shape, and can be uniform as well as waveform along the camber. Measurements involve Kiel probe traverses for different injection scenarios 0.5 axial chords downstream of the blades. Results show that, instead of performing uniform mass injection along the camberline, by selecting an appropriate waveform injection pattern one can reduce the total loss levels of the blade, including the tip leakage loss as well as the wake losses.

This thesis presents the results of an experimental study that investigates the effects of steady vortex generator jets (VGJs) integrated to a low pressure turbine blade to control the laminar separation bubble occurring on the suction surface of the blade at low Reynolds numbers. The injection technique involves jets issued from the holes located near the suction peak of the test blade which is in the middle of a five-blade low speed linear cascade facility. Three injection cases are tested with different blowing ratio values ranging from low to high. Surface pressure and particle image velocimetry (PIV) measurements are performed. The results show that steady VGJ is effective in eliminating the laminar separation bubble. Also it is observed that to have fully developed attached boundary layer, blowing ratio should be chosen accordingly since a very thin separation zone still exists at low blowing ratios.

According to the statistics about civil transportation aircraft Environmental Control system (ECS), the three-wheel high pressure water separation system (HPWS) and low pressure water separation system (LPWS) are the most common choices for the 150-seat airliners. Although the former has become the mainstream configuration for air conditioning pack, the latter is still used on Boeing 737-600/700. In order to compare the two configurations and choose the better one for a specific aircraft, simulation and analysis are done. The cabin heat load is calculated at first in order to calculate required engine bleed air mass flow. Then a specific aircraft is defined so that required structural dimensions and cabin comfort indexes can be obtained based on Airbus 320. Thirdly, the component models are built by Matlab/Simulink according to the fundamental knowledge of heat transfer and aerodynamics, the working principles and mechanical dimensions of the components, the ambient environmental parameters and some data from Airbus 320. Consequently, the complete system model can be assembled. After confirming the validity of the model by checking the required ram air mass flow and temperature deviation of the state points referred to Airbus 320, the simulation model is used to do analyze the specific aircraft. Finally, through comparing the different values of ram air mass flow and turbine expansion ratio, as well as the system mass, economic cost and reliability, the better configuration is selected. It can be summarized that the three-wheel LPWS requires less ram air mass flow (0.012kg/s) and a little lower expansion ratio (0.02) than the HPWS, and it also has lower weight (63% of HPWS), lower (83% of HPWS) cost and higher reliability (140% of HPWS), thus it is the suitable configuration for the specific aircraft.

L'évolution de l'électronique de puissance ces dernières années a entraîné une augmentation de la densité de puissance et une diminution du coût des onduleurs de tension à modulation de largeur d'impulsion (MLI). Ces évolutions ont répandu l'utilisation de convertisseurs de puissance pour les applications de variateurs de vitesse ce qui a permis le développement du concept d' " avion plus électrique ". Ce concept consiste à remplacer un des vecteurs énergétiques (pneumatique ou hydraulique) par l'énergie électrique. Cependant, le développement du réseau électrique a entraîné une augmentation de la tension embarquée, ce qui a conduit à un vieillissement prématuré des équipements électriques embarqués. La forme de tension appliquée, appelée "modulation de largeur d'impulsion" (MLI), est constituée de trains d'impulsions. Avec l'application de ces impulsions, la tension n'est plus distribuée de manière homogène le long du bobinage. Dans ce cas, on pourra observer d'importantes différences de potentiel entre les spires d'une même phase voire entre deux phases du bobinage. En outre, un autre paramètre important provient du type d'enroulement des moteurs utilisés par l'industrie. L'enroulement aléatoire est la technique de bobinage la plus courante pour les moteurs basses tensions car cette méthode présente un faible coût. Le risque induit par ce type d'enroulement est que la première et une des dernières spires de la première bobine peuvent être proches l'une de l'autre. Dans ce cas, jusqu'à 80% de la tension sera supportée par quelques dizaines de microns d'émail, et les systèmes d'isolation existants ne sont pas dimensionnés pour résister à de telles contraintes. L'utilisation de longs câbles reliant l'onduleur au moteur peut aussi provoquer des surtensions importantes aux bornes du moteur. Ce phénomène s'explique par le fait que le câble se comporte comme une ligne de transmission qui n'est pas adaptée en termes d'impédance au bobinage du moteur. De plus, ces importantes différences de potentiel associées à de faibles pressions, présentes dans les zones dépressurisées de l'aéronef, peuvent entraîner l'apparition de décharges partielles. Les décharges partielles sont des décharges électriques qui court-circuitent partiellement l'intervalle entre deux conducteurs. Il existe de nombreuses méthodes de détection bien connues pour les tensions AC et DC, cependant, la détection sous tension de type MLI dans des moteurs basse tension est beaucoup plus complexe. Les signaux de décharge partielle sont en effet intégrés dans le bruit électromagnétique généré par la commutation. Le but de cette thèse est donc de développer un procédé de détection et un procédé de filtrage permettant une détection non intrusive et en fonctionnement (on-line) des décharges partielles dans le domaine aéronautique afin de qualifier les systèmes d'isolation électrique utilisés dans les aéronefs. / The development of power electronics in recent years has led to increase power density and to decrease pulse width modulation (PWM) voltage inverter cost. These developments have expanded the use of power converters for variable speed drive applications which enabled the development of the concept of "more electric aircraft". This concept consists in replacing one of energy carriers (pneumatic or hydraulic) with electrical energy. However, the deployment of electrical energy has increased the onboard voltage, which leads to premature aging of onboard electrical equipment. The shape of the PWM voltage consists of pulse trains. With the application of these pulses, the voltage is no longer homogeneously distributed along the coil. In this case, large differences in potential between the strands are present. In addition, another important parameter derived from the winding type motor used in industry. The random winding is the most common technique for low voltage motors due to its lower cost. The risk generated by this type of winding is that the first and the last turns of the first coil can be facing one another. In this case, up to 80% of the voltage will be supported by a few tens of microns of enamel, and existing insulation systems are not designed to withstand such severe constraints. The use of long cable connecting the inverter to the motor can also cause significant overvoltage at the motor terminals. This phenomenon is explained by the fact that the cable behaves as a transmission line to which the motor coils is not adapted in terms of impedance. In addition, these large potential differences associated with low pressures in the depressurized areas of the aircraft, may cause the occurrence of partial discharge. Partial discharges are electrical discharges that short-circuited partially the gap between two conductors. There are many detection methods well known under AC and DC voltage, however, in the case of the detection under PWM like voltage in low-voltage motors, the detection is much more complex. Partial discharge signals are embedded in the electromagnetic noise generated by the switching. The aim of this thesis is to develop a detection method and filtering method enabling a non-intrusive and an "on-line" partial discharges detection in the aeronautical field in order to qualify the electrical insulation systems used in aircraft.

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.

Neste trabalho foi estudado o processo de moldagem por injeção em baixa pressão (LPIM do inglês: low-pressure injection molding) de pós cerâmicos submicrométricos para a produção de molas cerâmicas. O trabalho compreende a confecção de moldes e pequenas injetoras de laboratório, extração dos ligantes orgânicos utilizados durante a moldagem, a sinterização das peças e alguns ensaios preliminares para avaliar as propriedades mecânicas de molas cerâmicas. A LPIM apresenta muitas vantagens na produção de peças cerâmicas complexas, quando comparada à moldagem por injeção tradicional. Entretanto LPIM apresenta alguns problemas na remoção da mistura de ligantes que são maiores quando se confecciona peças cerâmicas preparadas com pós submicrométricos. Mas, por outro lado, a utilização destes pós permite a obtenção de corpos sinterizados com alta densidade e excelentes propriedades mecânicas. Os pós cerâmicos utilizados foram a alumina (Al2O3) e a zircônia (ZrO2), e o ligante principal utilizado foi a parafina. Moldes tubulares e moldes usinados multipartidos foram desenvolvidos para moldagem por injeção de molas de alumina e uma pequena injetora foi construída para injetar peças de zircônia. Os moldes tubulares mostraram-se pouco adequados. Por outro lado, a utilização do molde de latão multipartido, revestido com PTFE (politetrafluoretileno), melhorou o processo de fabricação de molas cerâmicas, possibilitando a confecção de quantidades maiores e com boa reprodutibilidade. No processo de sinterização das molas cerâmicas as distorções foram evitadas utilizando cilindros cerâmicos como suporte das molas. As molas de alumina e zircônia tiveram suas densidades e durezas medidas e estão de acordo com a literatura. Finalmente, foram feitos alguns ensaios preliminares de compressão com molas cerâmicas de alumina e zircônia para avaliar sua constante de mola e a carga máxima suportada antes da quebra. / Submitted by Marcelo Teixeira (mvteixeira@ucs.br) on 2014-05-15T16:08:53Z No. of bitstreams: 1 Dissertacao Raquel Andreola.pdf: 15781483 bytes, checksum: 33fd01d3cfc733b522788fea2e290b5a (MD5) / Made available in DSpace on 2014-05-15T16:08:53Z (GMT). No. of bitstreams: 1 Dissertacao Raquel Andreola.pdf: 15781483 bytes, checksum: 33fd01d3cfc733b522788fea2e290b5a (MD5) / In this work the low-pressure injection molding (LPIM) of submicrometer-sized ceramic powders was studied aiming to produce ceramic springs. The work comprised the production of molds and laboratory equipment for injection molding, the debinding of the organic vehicle used in the molding, the sintering of ceramic parts, and some preliminary experiments to evaluate the mechanical properties of the ceramics springs. The LPIM presents many advantages for complex ceramic parts production, in comparison with traditional high-pressure injection molding. However, LPIM has some difficulties associated to the debinding step, that are even greater for ceramic parts made with submicrometer-sized powders. But, on the other hand, the use of submicrometer-sized powders allows the production of sintered bodies with high density and better mechanical properties. The submicrometer-sized ceramic powders used in this work were alumina (Al2O3) and zirconia (ZrO2), and the main binder was the paraffin. Tubular molds and a multipart machined mold were developed for injection molding of alumina springs, and a little injection machine was build for injection molding of zirconia parts. The tubular molds had a limited performance. On the other hand, the multipart brass mold, coated with PTFE (polytetrafluorethylene), improved the ceramics spring molding process, making it possible to produce ceramic springs in greater quantities with good reproducibility. In the sintering process of the ceramic springs, major distortions of the parts were avoided using ceramic beams to support the springs. The alumina and zirconia ceramic springs had their measured density and hardness in good agreement with literature. Finally, some preliminary compression tests were performed with alumina and zirconia ceramic springs in order to evaluate their spring constant and maximum load before failure.

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.