Um estudo sobre a preparação metalográfica da liga de aluminio AA7075-T6

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

Implementação de um tuboexpansor na refinaria do Planalto Paulista – REPLAN com objetivo do aproveitamento da energia contida nos gases residuais do FCC – Fluid Catalytic Cracking na geração de energia elétrica

The steel type AISI 4130 (ultra-high strength steel) is an alloy of low carbon and its main alloying elements are chromium and molybdenum, which improves the toughness of the weld metal. It has numerous applications, especially where the need for high mechanical strength. It is widely used in equipment used by the aviation industry, such as cradle-tomotor, and this is the motivation for this study. Cots are of fundamental importance, because the engine supports and maintains balance in the fixed landing gear. This equipment is subjected to intense loading cycles, whose fractures caused by fatigue are constantly observed. Will be determined the effects caused by re-welding the structure of aeronautical equipment, and will also study the microstructure of the metal without welding. The studies will be done on materials used in aircraft, which was given to study. The results provide knowledge of microstructure to evaluate any type of fracture that maybe caused by fatigue. Fatigue is a major cause of aircraft accidents and incidents occurred, which makes the study of the microstructure of the metal, weld and re-solder the knowledge essential to the life of the material. The prevention and control of the process of fatigue in aircraft are critical, since the components are subjected to greater responsibility cyclic loading

Obtenção e caracterização de compósitos via RTM com alta fração de fibras de carbono processados à temperatura ambiente

After confirming the high specific mechanical properties of composite materials by scientific studies conducted over the last decades, one of the challenges of this new class of materials is the ability to achieve mass production at a more affordable cost, which has become indispensable. The Resin Transfer Molding (RTM) is an excellent method for manufacturing composite materials. Despite being a process widely used by international companies in the production of high performance structural composites, only a short time the national aviation industry has shown interest in implementing this type of processing to more complex structures and greater structural responsibility. In aeronautical projects, the reproducibility and the relative low cost of this process, several studies have been performed in Brazil for learning and perfecting this technique. This process is suitable for producing polymer components both simple as complex geometry, and allows to achieve consistent thickness, with high quality finish and without limiting range. Polymeric composite components for the high mechanical stress applications such as aircraft structures, satellites, etc., require a strict control of volume fractions of the composite constituents, beyond the knowledge of their mechanical and thermal properties. Therefore, in this experimental work degree study on the mechanical, thermal and of porosity composites processed by RTM processed characterization was performed. This characterization was performed targeting a possible aerospace application of this composite material. For the production of composites, process equipment (RTM RTM injector Radius 2100cc) was used. The processed carbono/epoxy composites were characterized via flexure tests mechanically and thermally analysis via DMA, DSC and TGA. To determine the volume fraction of fibers, the composite samples were analyzed via matrix digestion (ASTM D3171) ... (Complete abstract click electronic access below)

Avaliação da colagem de suportes utilizados para fixar cabos elétricos em aeronaves

The most usual method to fix supports that hold the vast majority of electrical cables on an aircraft is accomplished by using, for this purpose, rivets. However, this procedure may some cause some inconveniences such as the need of effecting holes in the structure that is intended to fix these supports, thus decreasing resistance of the structure. In order to have an alternative to seek an increase in the performance of structured materials, the aircraft industry, like other industries, have been studying the use of collage as a method of replacing this usual forms. Against this backdrop, this paper aims to assess the strength and durability of a joint bonded using the adhesive EA9394, manufactured by company Henkel Corporation, and perform a careful survey of the mechanical performance of riveted structures, taking into account different types of conditioning environment and thus create a database that can be used by the aerospace industry

Desenvolvimento de aplicativo de análise técnica e econômica para adaptação de uma roda d’água acionada por cima para geração de energia elétrica no meio rural

The steel type AISI 4130 (ultra-high strength steel) is an alloy of low carbon and its main alloying elements are chromium and molybdenum, which improves the toughness of the weld metal. It has numerous applications, especially where the need for high mechanical strength. It is widely used in equipment used by the aviation industry, such as cradle-tomotor, and this is the motivation for this study. Cots are of fundamental importance, because the engine supports and maintains balance in the fixed landing gear. This equipment is subjected to intense loading cycles, whose fractures caused by fatigue are constantly observed. Will be determined the effects caused by re-welding the structure of aeronautical equipment, and will also study the microstructure of the metal without welding. The studies will be done on materials used in aircraft, which was given to study. The results provide knowledge of microstructure to evaluate any type of fracture that maybe caused by fatigue. Fatigue is a major cause of aircraft accidents and incidents occurred, which makes the study of the microstructure of the metal, weld and re-solder the knowledge essential to the life of the material. The prevention and control of the process of fatigue in aircraft are critical, since the components are subjected to greater responsibility cyclic loading

Usinagem da liga de níquel inconel 718 com pastilhas de cerâmica

The machining of super alloys resistant to high temperatures such as nickel alloys, inconel 718 specifically, is a very difficult job to obtain improvements in the process, due to the difficulty of machining at high cutting speeds, the use of these alloys in industries showed great developments in recent years, its application in aeronautical industry spread being used in vane turbo, compressor parts, props and set elements. The automotive, chemical, medical and others also took advantage of the great features of inconel 718 and has used the material. The high temperature resistant alloys have high machining difficulty, a fact that is associated with high cutting forces generated during machining which result in high temperatures. High levels of temperatures can cause deterioration of the cutting edge, with subsequent deformation or breakage, wear most common obtained in machining such materials are flank wear the formation of built-up edge for cutting and notch wear. The experimental part of the work consists in machining of nickel-based alloy Inconel 718 heat treated for hardness, using a tool based ceramic silicon nitride Sandvik (Si3N4) in order to compare the best results obtained in the master's thesis of SANTOS (2010) who used a tool ceramics also the basis of silicon nitride which was developed in the doctoral thesis of SOUZA (2005). Assays were performed on a CNC lathe and was noted for each cutting edge results obtained. Tests were made starting from an initial condition of the tool with cutting speed of 200 m/min, feed 0.5 mm and 0.5 mm depth of cut was reduced cutting speed for the subsequent tests with the same conditions of feed and depth of cut. The tool presented wear instant under two 200 m/min and 100 m/min, premature rupture of 50 m/min and finally cut provided with difficulty... (Complete abstract click electronic access below)

Estudo do aumento no diâmetro do corpo de um rebite a ser cravado em furos acima da tolerância de projeto

In this work are discussed the main types of rivets, their characteristics and applicability within the Aeronautical Industry branch. Here are highlighted the solid rivets, showing off its layout, forms and limits of installation, that are required by aviation regulators. The riveting is a popular and simple procedure of fixing and joining two or more parts, and like any other manufacturing process is subject to process deviations that in some situations are beyond the limits of tolerance. One of these deviations is when the hole diameter exceeds the one proposed in project and which is limited by the rule of edge distance. The overall objective here is to study a possible solution to this problem: the installation of a rivet that has his diameter previously increased by compression. Observe the hole filling after riveting, detect the presence of cracks, discover the yield curve of the fasteners and their the crushing limits for failure prediction are tools used to verify this proposal. They demonstrate, at the end of study, the inefficiency of this procedure, with results that go against the safe fixing of parts in a structure

Precificação no Setor de serviço

Given the competitive reality of the globalized market, companies are compelled to develop strategic aspects of the management process, in order to ensure their survival. Among the strategic aspects is the price formation process, whose reasoning occurs mainly of adoption through cost system. Knowledge of costs and expenses provides conditions for the company to position itself strategically in the market, being able to follow the price of competition and sometimes even surpass them, called, more and more attention with regard to price formation. This study aims to identify the best price to be transferred to the market. To this end, were approached concept of pricing and its components, their strategies and pricing objectives, as well as the influence of demand on price formation, as well as the added value the brand and quality; and even a careful analysis of the price established by the said company in the service offered. We used the method of literature review and case study in the company ESA international aeronautical industry. Thus, we sought to explain about the main concepts for pricing in order to support decision making

Otimização do processo de soldagem por resistência elétrica em compósitos PEI/fibras contínuas para aplicações aeronáuticas

Pós-graduação em Engenharia Mecânica - FEG

Avaliação dos parâmetros tempo, corrente e pressão na soldagem por resistência elétrica de compósitos PEI/fibras contínuas: influência na resistência mecânica

Fundação de Amparo à Pesquisa do Estado de São Paulo (FAPESP)

Análise numérica e experimental de juntas aeronáuticas rebitadas sob solicitação estática.

Uniões por prendedores são elementos amplamente utilizados na indústria aeronáutica para a união de partes constituintes da aeronave. Contudo, devido à sua geometria e aos carregamentos sofridos, estes elementos estão frequentemente sujeitos a falhas por fadiga. Assim, para um projeto e dimensionamento bem executado dessas juntas, é necessário conhecer seu comportamento mecânico e o campo de tensões ao qual estão sujeitas. O método dos elementos finitos certamente atende a estas necessidades; porém, o uso de elementos sólidos tridimensionais para a representação destas uniões pode levar a análises demasiadamente demoradas e custosas, sendo desejável o uso de modelos mais simplificados. Nesse trabalho, juntas de topo assimétricas são modeladas pelo método dos elementos finitos, utilizando tanto elementos sólidos tridimensionais quanto elementos de casca, com o objetivo de encontrar um modelo relativamente simples que apresente resultados satisfatórios e requeira um menor tempo de solução. Os resultados numéricos obtidos são comparados com resultados experimentais, que utilizam extensômetros e fotoelasticidade.

Fadiga em elementos tubulares de matriz epoxídica reforçada com fibras de carbono sujeitos a solicitações de torção e flexão

Os materiais compósitos são materiais em expansão. Revolucionaram a indústria aeronáutica e actualmente difundem-se nos mais variados nichos industriais, mesmo nas aplicações mais comuns. Têm uma grande aplicação em elementos estruturais, sendo submetidos a estados de tensão e deformação multiaxiais. Os elementos tubulares de matriz epoxídica reforçada com fibras de carbono são exemplos típicos de componentes. No entanto, devido ao aparecimento relativamente recente destes materiais, os modelos de fadiga utilizados nos materiais comuns mostraram-se pouco realistas. Surgiu assim a necessidade de adaptar e elaborar novos modelos de fadiga, com resultados mais satisfatórios na previsão da vida dos componentes, recorrendo a ensaios laboratoriais. No presente estudo experimental, recorrendo a um sistema adequado de amarras, foram realizados ensaios de torção e de flexão pura, quer estáticos, quer dinâmicos, numa máquina servo-hidráulica convencional. Nos ensaios de fadiga foram consideradas duas razões de tensões (R=0,05 e R=0,3). Foram também realizados ensaios de fadiga com carregamentos de flexão-torção em fase sob amplitude de tensão constante, com as mesmas razões de tensões, considerando o momento flector igual ao momento torsor (B=T). Foi avaliado o efeito da tensão média, recorrendo aos critérios de Gerber e Goodman, os quais se apresentaram satisfatórios, tendo em conta o número reduzido de estudos efectuados. Já nos ensaios biaxiais, o critério de Tsai–Hill mostrou-se erróneo perante os resultados experimentais. No entanto, após ter sido aplicado um ajustamento, os resultados melhoraram. Foi também estudado o comportamento elastoplástico dos corpos de prova em todos os ensaios.

Utilização da metodologia six sigma no âmbito da formação em manutenção aeronáutica

O Sector da Aviação Civil tem sofrido diversas alterações nos últimos anos. No entanto, os padrões de segurança têm forçosamente de ser mantidos. As alterações ao nível da regulamentação e consequente racionalização de todo o Sector abrangem o ramo da Manutenção de Aeronaves, que é alvo de especial atenção. A metodologia Six Sigma tem vindo a ser desenvolvida desde os anos 80 do século passado, altura em que teve a sua origem no sector da Indústria, no entanto, o seu desenvolvimento no sector dos serviços, onde se inclui a formação profissional em manutenção aeronáutica, tem vindo a crescer. O presente estudo tem o objectivo de avaliar o contributo da metodologia Six Sigma no âmbito da formação em Manutenção Aeronáutica numa MTO (Maintenance Training Organisation), abordando algumas formas para a aplicação dos passos DMAIC (Define-Measure-Analyze-Improve-Control) na empresa TAP MTO. Explora-se a potencialidade desta metodologia na identificação e na decomposição dos problemas até à sua complexidade mínima, facilitando assim a resolução dos mesmos. Verifica-se que a aplicação da metodologia Six Sigma pode ser feita sem o recurso a alterações na estrutura orgânica de uma Organização, trazendo consigo inúmeros benefícios, tanto financeiros como operacionais. A metodologia aplicada não rompe com os recursos e metodologias já existentes. Permite, no entanto, uma “reciclagem” dos mesmos, aumentando a sua importância e utilidade, sem necessidade da reformulação de todo o processo. Existe ainda uma alteração na abordagem de dificuldades e o envolvimento dos cargos de Gestão mais elevados no processo de mudança.

O mercado doméstico de transporte aéreo de passageiros: modelo de escolha de capacidade empregada em função da ação do regulador e da estrutura da indústria

O presente tabalho apresenta um modelo destinado à análise do mercado doméstico de transporte aéreo de passageiros. O modelo analisado permite acompanhar as escolhas ótimas das companhias aéreas quanto ao número de vôos ofertados e passageiros transportados diante das alterações no valor das tarifas promovidas pelo reguldor, tanto em equilibrio competitvo quanto monopolista e, alternativamente, caso a indústria atue como um oligopólio. Neste último caso, o modelo analisado permite que o equilíbrio da indústria seja mensurado em conjunto com parâmetros conjecturais de comportamento das firmas.

Programação esportiva na TV Brasil : a influência da ideologia e indústria cultural

Universidade Estadual de Campinas . Faculdade de Educação Física