297 resultados para Aluminio


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Coordenação de Aperfeiçoamento de Pessoal de Nível Superior (CAPES)

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The approach of the subject matter in this work relies on the fact that the reliability of methods for performance analysis of materials proves critical for the result. This work focused on the development and presentation of the methodology for lifting probability curves for fatigue test (SN) according to standard E739, this focus is justified by the fact that the results in fatigue test show considerable dispersion making it difficult to reading and interpretation of data, this dispersion arises because the phenomenon of rupture is strongly influenced by internal characteristics of the material, we can then have much data ranging from test to test. Thus we set out originally for a brief study of aluminum alloys in question, as well as the treatments to which they were subjected. We also studied the behavior of materials when subjected to cyclic loading, which configures process of fatigue failure, and even fatigue test method in question. This statistical analysis is based on the ASTM E739 standard, so its contents was studied in detail so that we could present in detail the methodology and raise SN curves for different aluminum alloy 7012 subjected to fatigue test. Data were collected from tests conducted in the department of materials from two samples of aluminum alloy 7012 solubilized and precipitated by different time intervals and assayed temperature fatigue-type traction-compression, these data were then analyzed and used to survey curves using the base as E739. After lifting the curve analyzed the characteristics of the test samples and their correlation with the test results. We confirmed the effectiveness of the method of statistical analysis by ASME E739, which allowed the reading of data without this method would be very difficult to have a reading and comparison of the results for the two types... (Complete abstract click electronic access below)

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The increasing technological innovation and demand for materials with better properties boosts research into new materials and new alloys. To do so, aluminum alloys are being developed, among them the AA7075-T6, having many applications in aerospace and military industries, machinery and equipment, molds for plastic injection and structures. To study and understand the properties, characteristics and especially the microstructure of the material, the metallographic preparation is essential. This paper presents new methodologies to achieve the metallography of samples of scrap alloy AA7075-T6, with emphasis on methods of polishing. For the five samples, the best results were those with specific grinding, the samples only going down on the sander. For polishing, the most effective method so far has been using the polishing cloth 16.3, of ATM enterprise, solution of diamond 3 μm, solution of diamond 1 μm, and colloidal solution of OP-S. For the etching, the reactive agent used was phosphoric acid (H3PO4) 85% P.A., as 90% in the proportion of distilled water to 10% acid. The best results were obtained in the attacks of 300 and 240 seconds, revealing the grain boundaries in most areas. Methodologies need more studies and more tests, but the results have proved to be satisfactory

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The Sanding is a complex process involving many variables that affect the quality of the part produced, working mainly in the timber industry in the production of panels (MDF, MDP, HDF, etc...) and furniture. However, these industries use the sanding process empirically, not optimizing it. The aim of this study was to compare the behavior of sandpaper white aluminum oxide (OA-white) and Black silicon carbide (SiC-black), analyzing variables in the process as: strength, power, emission, vibration, wear particle size of sanding, and its consequences on the surface finish of the workpiece. Made the process of plane grinding samples of Pinus elliottii, processed in parallel to the fibers, which were sanded with sandpaper grain OA white and black 3-SiC abrasive conditions (new, moderately eroded and severely eroded) grain sizes in 3 (80, 100, and 120 mesh). 6 replicates was performed for each condition tested. Each trial was captured output variables of the sanding process: strength, power, emission and vibration. With two stages totaling 108 trials. After the sanded samples, it has the same surface quality by raising the surface roughness Ra. Through experiment, it can be concluded that abrasives OA-white tended to have higher strength, power, emissions and less vibration in the sanding process, compared to the SiC-black. However, surface finish exhibited similar to the particle size of 80 to 100 mesh, worn abrasive conditions. However, the particle size of 120 mesh, obtained by the roughness of sandpaper OA-bank was higher compared to SiC-black to all conditions of sandpaper due to its toughness

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The aluminium alloys are used in many fields because of their versatility combined with the excellent aluminium’s properties, mentioned in the study. This study aims to compare the performance of polished Hard Metal, Hard Metal covered with TiB2 and High Speed Steel (HSS) tools, at the aluminium 2024 alloy’s turning, as a function of variation of some turning parameters such as: feed, depth of cut and cutting speed; and study the surface finish and the required power during turning by processing the output data, like analyze the chip’s features for each used tool. The results provide information of the tool’s material effects, when submitted to different turning conditions, about the output variable in question. In this way, it was possible to notice that although the Hard Metal covered with TiB2 tool has provided the better surface finish, the chip’s features were better when the turning was accomplished by the Polished Hard Metal tool. In relation to the required turning’s power, the lowest consumption occurred with the High Speed Steel tool

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Dependiendo de la conexión entre sus poros, las espumas metálicas se clasifican en espumas de poro abierto o poro cerrado. La mayoría de las espumas que se comercializan actualmente son espumas de poro cerrado. Sin embargo, para algunas aplicaciones son más apropiadas las espumas de poro abierto. En este trabajo, se estudia el coeficiente de absorción en tubo de impedancia de espumas de aluminio de poro abierto fabricadas mediante el proceso de infiltración. Estas espumas se caracterizan por una estructura muy homogénea y por un elevado valor del coeficiente de absorción a bajas frecuencias cuando se combinan con una cámara de aire

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Generalmente los elementos estructurales metálicos de las aeronaves se ubican en zonas de carga crítica, en la mayoría de los casos, estos elementos son conformados mediante procesos de mecanizado. La vida a fatiga de estos componentes es una propiedad dinámica muy importante que puede verse intensamente afectada por las condiciones superficiales producidas durante el proceso de mecanizado. En este trabajo se lleva a cabo un primer estudio de la influencia de los parámetros de corte en la resistencia a la fatiga de piezas torneadas de la aleación de aluminio aeronáutico UNS A92024-T351. Se ha prestado especial atención a la relación con el acabado superficial evaluado a partir de la rugosidad media aritmética

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Uno de los retos actuales aún pendiente de lograr trabajando con espumas de aluminio, es el desarrollo de métodos de unión fácilmente reproducibles a nivel industrial que permitan la unión de espumas de aluminio entre sí o con otros componentes tipo pletinas, para así poder fabricar piezas de mayor tamaño o con formas complejas, a la vez que se conserven las propiedades y características principales de las espumas de aluminio, tanto en la zona principal de unión o cordón, como en la interfase y zona afectada térmicamente, que se encuentran anexa. Los actuales procesos de unión más utilizados con espumas de aluminio, se basan principalmente en adhesivos y uniones mecánicas. Estas soluciones a priori válidas, añaden problemas técnicos a determinadas aplicaciones de las espumas que frenan la completa integración de estos materiales en un entorno de fabricación flexible y global. Por esta razón, los actuales procesos de producción de las espumas de aluminio se restringen a determinadas ofertas hechas a la medida del cliente, no pudiendo atender por falta de soluciones, a una gran parte del potencial mercado de estos materiales. En el presente trabajo de investigación se han desarrollado y caracterizado diferentes métodos de unión de espumas de aluminio, en configuración a tope y de espumas de aluminio con pletinas en configuración a solape, basados en procesos por soldeo térmico. One of the current challenges even pending of being achieved working with aluminium foams, is the development of easily reproducible methods at industrial level that allow the joint of aluminium foams between them or with other elements as for example aluminium plates for making bigger pieces or with more complex forms, remaining simultaneously in the weld bead the properties and main characteristics of aluminium foam, so much in the joint area or interface, since in the affected closer thermal zone. Currently, the most used joint processes for applying to aluminium foams are based mainly on adhesives and mechanical joins. These solutions initially valid, add technical problems to certain aluminium foams applications, which stop the complete integration of these materials in a more flexible and global manufacture environment. For this reason, current aluminium foam manufacturing processes are restricted to certain offers done to a specific customer requirement, not being able to attend for lack of available solutions, to a great potential market of these materials. In the present work, different joint methods between aluminium foams and between aluminium foams and plates for butt and lap configurations have been developed and characterized based on thermal welding processes.

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Con este trabajo se pretende determinar la relación entre las características físicas y mecánicas y la estructura para espumas de aluminio de Al12Si y AA6061 obtenidas por pulvimetalurgia utilizando probetas prismáticas de dimensiones diecisiete por diecisiete por sesenta milímetros. De su estudio mecánico y de análisis de imagen se concluye que las probetas cuyas propiedades físicas y mecánicas están moderadamente por encima de la media poseen mayor número de poros medianos y paredes de poro más gruesas. Por el contrario, las propiedades resultan inferiores cuando se presentan estructuras con un mayor número de poros medianos. Aquellas espumas con estructuras obtenidas por una espumación incompleta presentan una menor porosidad y por ello mayores densidades. En aquellos casos donde la estructura presenta una elevada presencia de poros grandes, sus propiedades mecánicas disminuyen. ABSTRACT With this work we are trying to determine the relation between physical and mechanical characteristics and its structure, for Al12Si and AA6061 aluminium foams, obtained by podwer metallurgy. Aluminium foam samples with dimensions of seventeen per seventeen per sixty millimeters were used. After its mechanical and image analysis study, we conclude that samples whose physical and mechanical properties are moderately over the average, they have a major proportion of medium pores and thicker pore walls. Otherwise, properties result to be inferior when a major number of medium pores structures are presented. Those foam structures obtained with an incomplete foaming process show a lower porosity, and so higher densities. Also, properties decrease in those cases in which the structure presents a high presence of big pores.