Análise do efeito higrotérmico no comportamento em fadiga de compósitos de PPS/fibras de carbono

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

Estudo da adesividade (TACK) de pré-impregnados de resina epóxi reforçada com fibras de carbono

Coordenação de Aperfeiçoamento de Pessoal de Nível Superior (CAPES)

Estudo dos critérios de falhas em compósitos PPS/fibras de carbono utilizando elementos finitos

Coordenação de Aperfeiçoamento de Pessoal de Nível Superior (CAPES)

Otimização da retificação tangencial plana de compósitos plásticos reforçados com fibras de carbono

Pós-graduação em Ciência e Tecnologia de Materiais - FC

Monitoramento do processo de densificação de compósitos termoestruturais de carbono reforçado com fibras de carbono por tomografia computadorizada e resistividade elétrica

Coordenação de Aperfeiçoamento de Pessoal de Nível Superior (CAPES)

Estudo das intempéries nas propriedades mecânicas e viscoelásticas de compósitos PPS/Fibras de carbono e EPOXI/Fibras de carbono de uso aeronaútico

Coordenação de Aperfeiçoamento de Pessoal de Nível Superior (CAPES)

Obtenção e caracterização de compósitos de fibras de carbono/PEKK com aplicações aeronaúticas

Coordenação de Aperfeiçoamento de Pessoal de Nível Superior (CAPES)

Estudo da aplicabilidade do sistema pultrudado de fenólica/fibras de carbono em cabos condutores

Pós-graduação em Engenharia Mecânica - FEG

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)

Estudo da superfície de fibras de carbono após tratamento de implantação iônica por imersão em plasma (3IP)

In this work, plasma immersion ion implantation (PIII) treatments of carbon fibers (CFs) were performed in order to induce modifications of chemical and physical properties of the CF surface aimed to improve the performance of thermoplastic composite. The samples to be treated were immersed in nitrogen or air glow discharge plasma and pulsed at −3.0 kV for 2.0, 5.0, 10.0, and 15.0 min. After PIII processing, the specimens were characterized by atomic force microscopy (AFM), scanning electron microscopy, Raman spectroscopy, and X-ray photoelectron spectroscopy (XPS). After CFs treatments, the CF/Polypropylene (PP) composites were produced by hot pressing method. Surface morphology of as-received CFs exhibited some scratches aligned along the fibers due to the fiber manufacturing process. After both treatments, these features became deeper, and also, a number of small particles nonuniformly distributed on the fiber surface can be observed. These particles are product of CF surface sputtering during the PIII treatment, which removes the epoxy layer that covers as-received samples. AFM analyses of CF samples treated with nitrogen depicted a large increase of the surface roughness (Rrms value approximately six times higher than that of the untreated sample). The increase of the roughness was also observed for samples treated by air PIII. Raman spectra of all samples presented the characteristic D- and G-bands at approximately 1355 and 1582 cm−1, respectively. Analysis of the surface chemical composition provided by the XPS showed that nitrogen and oxygen were incorporated onto the surface. The polar radicals formed on the surface lead to increasing of the CF surface energy. Both the modification of surface roughness and the surface oxidation contributed for the enhancement of CF adhesion to the polymeric matrix. These features were confirmed ... (Complete abstract click electronic access below)

Avaliação dos efeitos ambientais nas propriedades do compósito de poliamida 6,6/fibras de carbono

This graduation work done study of polyamide 6.6/composite carbon fibres, since its processing, characterization of the main properties. Besides the influence of temperature, UV radiation, salt spray and moisture on the mechanical and viscoelastic behavior. To achieve this goal, the first composite was processed from the heat compression molding using known variables of the process and using the empirical method to find the best value for other parameters. The method processing molding was chosen because it common in composites processing in order to evaluate the influence of crystallinity of the properties that influence the mechanical and viscoelastic behavior laminates. From the obtained laminate specimens were evaluated in weathering, such as: in hygrothermal chamber, UV, salt spray and thermal shock. In another step, the effect produced by these constraints were evaluated by optical microscopy, ultrasound, dynamic mechanical analysis and vibration tests. This project was conducted at the Department of Technology and Materials of UNESP in Guaratingueta, where all the equipment and techniques for the implementation of this project met available. After the tests proved the applicability of the composite polyamide 6.6/carbon fibers in aeronautical applications with resistance the main climatic influences

Estudo da modificação superficial de fibras de carbono por meio de tratamentos a plasma para o aumento da adesão na interface de compósitos fibra de carbono/PPS

Pós-graduação em Engenharia Mecânica - FEG

Comportamiento de vigas de hormigón reforzadas a cortante con tejidos de fibras de carbono pegados con resina epoxi

El objetivo principal de este trabajo ha sido estudiar el comportamiento de vigas de hormigón, reforzadas a cortante con tejidos de fibra de carbono pegados con resinas epoxi. Para conseguir este objetivo se han planteado objetivos parciales como el análisis de la fisuración y de los movimientos en las vigas reforzadas. La metodología empleada ha sido principalmente experimental, realizándose una serie de diez vigas de hormigón en masa o armado. Se han comparado los resultados experimentales con los teóricos, obtenidos mediante la formulación analítica existente, como la recomendada por el fib Bulletin 14. Los resultados obtenidos demuestran que las vigas reforzadas ofrecen un comportamiento significativamente superior al de las vigas sin refuerzo, tanto en el valor de las cargas últimas como en la ductilidad de las piezas. Además se puede concluir que en todos los casos estudiados la rigidez prevista hasta la fisuración de las vigas es superior a la obtenida experimentalmente. Además las vigas reforzadas a cortante con tejido de fibra de carbono poseen una ductilidad superior a la de las vigas sin reforzar

Comportamiento de vigas de hormigón reforzadas a cortante con tejidos de fibras de carbono o basalto

El objetivo principal ha sido estudiar el comportamiento de vigas de hormigón reforzadas a cortante con tejidos de fibra de carbono o basalto pegados con resinas epoxi. Se han planteado objetivos parciales como el análisis de la fisuración y de los movimientos en las vigas y la comparación del comportamiento mecánico de los sistemas de refuerzo estudiados. La metodología empleada ha sido experimental, realizándose vigas de hormigón en masa reforzadas inferiormente con tejido de fibra de carbono. Las vigas se han reforzado a cortante con tejidos de fibra de carbono o basalto. Se han comparado los resultados experimentales con los teóricos, obtenidos mediante la formulación analítica existente. Los resultados demuestran que las vigas reforzadas ofrecen un comportamiento significativamente superior al de las vigas sin refuerzo, tanto en el valor de las cargas últimas como en la ductilidad de las piezas. Además la rigidez prevista hasta fisuración es superior a la obtenida experimentalmente. Los resultados obtenidos nos permiten concluir que de la formulación aditiva propuesta por el Fib Bulletin 14 no se obtienen buenos resultados y que la formulación existente en diversas normativas vigentes para el cálculo de la resistencia a cortante del hormigón resulta conservadora.

Comportamiento de vigas de hormigón reforzadas a cortante con tejidos de fibras de carbono o basalto pegados con resina epoxi

Tanto en estructuras de edificación como de obra civil cada día resulta más frecuente la necesidad de su refuerzo, bien por problemas asociados a patologías o por el aumento de las cargas asociado generalmente a un cambio de uso. El objetivo principal de este trabajo ha sido estudiar el comportamiento de vigas de hormigón, reforzadas a cortante con tejidos de fibra de carbono o basalto pegados con resinas epoxi. Para conseguir este objetivo se han planteado objetivos parciales como el análisis de la fisuración y de los movimientos en las vigas reforzadas con polímeros reforzados con fibras (FRP) y la comparación del comportamiento mecánico de los sistemas de refuerzo estudiados.