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Resina ep?xi aplicada a capacitores : influ?ncia de diferentes agentes de curaSilva, Rafael Bitello 16 July 2018 (has links)
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Previous issue date: 2018-07-16 / Coordena??o de Aperfei?oamento de Pessoal de N?vel Superior - CAPES / In this study the influence of different commercial curing agents of epoxy resin on film capacitors encapsulation was evaluated. A formulation with DGEBA epoxy resin was used with three different curing agent types: anhydride base, aliphatic amine base and polyamidoamine base. The curing reaction kinetic analysis of each epoxy system was performed by Osawa dynamic method by DSC according ASTM E968. The thermal properties of the epoxy systems were checked by TGA and DSC while the mechanical properties were measured by Shore D hardness and IZOD impact strength, also the a characterization by SEM was performed. The epoxy systems performance in capacitor was verified by qualification tests for film capacitors for automotive application based in AEC-Q200 D, as: exposure to the maximum capacitor operating temperture, exposure to thermal cycles and exposure to humidity. The capacitors were characterized by the capacitance variation while the effects in the epoxy systems were checked by their thermal and mechanical properties change. The systems based on aliphatic amine and polyamidoamine had lower activation energy and higher reaction velocity than the anhydride system. The performance of the capacitor against humidity was similar between the evaluated systems showing low loss of capacitance after the test, whereas against thermal cycles, even the aliphatic amine and polyamidoamine base systems were not affected by reduction of mechanical properties, they had their performance affected by cracks arising. Regarding the performance under exposure to the maximum operating temperature, the anhydride system presented the lowest capacitance loss in the capacitor, followed by the samples with polyamidoamine and aliphatic amine, respectively, which showed a significant reduction of the mechanical properties after prolonged exposure to the temperature of the test. / Neste estudo avaliou-se a influ?ncia de diferentes agentes de cura comerciais de resina ep?xi no encapsulamento de capacitores de filme. Foi utilizado uma formula??o de resina ep?xi DGEBA (diglicidil ?ter de bisfenol-A) com tr?s tipos diferentes de agente de cura: base anidrido, base amina alif?tica e base poliamidoamina. A an?lise da cin?tica da rea??o de cura de cada sistema ep?xi foi realizada pelo m?todo din?mico de Osawa, por DSC conforme ASTM E968. As propriedades t?rmicas dos sistemas ep?xi foram determinadas por TGA e DSC enquanto que as propriedades mec?nicas foram medidas atrav?s de dureza Shore D e resist?ncia ao impacto IZOD, al?m disto foi realizado caracteriza??o por MEV. O desempenho dos sistemas ep?xi no capacitor foi verificado pelos ensaios de qualifica??o de capacitores de filme para aplica??o automotiva baseados na norma AEC-Q200 D, sendo estes: exposi??o a temperatura m?xima do capacitor, exposi??o a ciclos t?rmicos e exposi??o a umidade. Os capacitores foram caracterizados pela varia??o de capacit?ncia enquanto que os efeitos nos sistemas ep?xi foram acompanhados pela altera??o em suas propriedades t?rmicas e mec?nicas. Os sistemas a base de amina alif?tica e poliamidoamina apresentaram menor energia de ativa??o e maior velocidade de rea??o que o sistema anidrido. O desempenho do capacitor frente a umidade foi similar entre os sistemas avaliados com baixa perda de capacit?ncia ap?s o ensaio, enquanto que frente aos ciclos t?rmicos, mesmo n?o apresentando redu??o de propriedades mec?nicas os sistemas base amina alif?tica e poliamidoamina tiveram seu desempenho afetado pelo aparecimento de trincas. Em rela??o ao desempenho sob exposi??o ? temperatura m?xima o sistema anidrido foi o que apresentou menor perda de capacit?ncia no capacitor, seguido das amostras com poliamidoamina e amina alif?tica, respectivamente, sendo que estas apresentaram redu??o significativa das propriedades mec?nicas ap?s exposi??o prolongada a temperatura do ensaio.
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Influ?ncia do retardante de chamas nas propriedades mec?nicas e flamabilidade em comp?sitos polim?ricos de ep?xi/fibra de curau?Rocha, Itailza Gomes da 08 September 2015 (has links)
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Previous issue date: 2015-09-08 / Atualmente se observa uma grande busca por materiais originados de fontes renov?veis. As fibras vegetais como refor?o para matrizes polim?ricas, tem sido uma alternativa para substituir fibras sint?ticas, por serem biodegrad?veis e de baixo custo. Este trabalho objetiva desenvolver um material comp?sito de resina ep?xi refor?ado com fibra de curau? e aditivo retardante de chama de alumina trihidratada (hidr?xido de alum?nio - Al(OH)3), que foi utilizado em propor??es de 10%, 20% e 30% do volume total do comp?sito. As fibras de curau? passaram por um processo de limpeza com um banho alcalino de hidr?xido de s?dio (NaOH), paralelizadas atrav?s de cardagem manual e cortadas de acordo com o comprimento predefinido. Foram moldados comp?sitos com fibras de 30cm e com fra??o volum?trica de 20% de fibra no Lossy Mould. Os comp?sitos foram preparados no Laborat?rio de Engenharia T?xtil da UFRN. Os testes de resist?ncia ao fogo foram realizados no laborat?rio de engenharia de materiais da UFRN. Para medir o desempenho do material, foram realizados ensaios de resist?ncia ? tra??o e flex?o, com as amostras que foram posteriormente analisadas no aparelho de Microscopia Eletr?nico de Varredura (MEV). Os comp?sitos apresentaram bom desempenho mec?nico, e foi observado que a adi??o do agente retardante de chama influenciou nas propriedades mec?nicas, e em alguns casos, deixando o comp?sito mais fr?geis a ruptura. Esses resultados mec?nicos foram submetidos ao teste estat?stico Qui-Quadrado ao n?vel de signific?ncia de 5% para verificar poss?veis diferen?as entre ao grupos de comp?sitos. O teste de flamabilidade foi realizado baseado na norma Underwriter's Laboratory 94 e o material apresentou um resultado satisfat?rio, tendo a sua taxa m?dia de queima (mm/min) diminuindo com o aumento da adi??o do retardante de chamas nos comp?sitos. / Currently, there is a great search for materials derived from renewable sources. The vegetable fibers as reinforcement for polymer matrixes, has been used as an alternative to replace synthetic fibres, being biodegradable and of low cost. The present work aims to develop a composite material with epoxy resin reinforced with curau? fibre with the addition of alumina trihydrate (aluminum hydroxide, Al(OH)3) as a flame retardant, which was used in proportions of 10 %, 20% and 30% of the total volume of the composite. The curau? fibers have gone through a cleaning process with an alkaline bath of sodium hydroxide (NaOH ), parallelized by hand and cut carding according to the default length . They were molded composites with fibers 30cm. Composites were molded in a Lossy Mold with unidirectional fibres in the proportion of 20% of the total volume of the composite. The composites were prepared in the Chemical Processing Laboratory of the Textile Engineering Department at UFRN. To measure the performance of the material, tests for the resistance to traction and flexion were carried out. with samples that were later analyzed in the Electronic Microscopy Apparatus (SEM ). The composites showed good mechanical properties by the addition of flame retardant and in some cases, leaving the composite more vulnerable to breakage. These mechanical results were analyzed by chi-square statistical test at the 5% significance level to check for possible differences between the composite groups. Flammability testing was conducted based on the standard Underwriters Laboratory 94 and the material showed a satisfactory result taking their average burn rate (mm / min) decreasing with increasing addition of the flame retardant composite.
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Mecanismos de dano em laminados de carbono/ep?xi sob fadiga e envelhecimento higrot?rmicoFulco, Ana Paula Pereira 30 November 2017 (has links)
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Previous issue date: 2017-11-30 / Conselho Nacional de Desenvolvimento Cient?fico e Tecnol?gico (CNPq) / Coordena??o de Aperfei?oamento de Pessoal de N?vel Superior (CAPES) / Materiais comp?sitos de matriz polim?rica refor?ados com fibras de carbono utilizados em estruturas aeron?uticas e aeroespaciais est?o frequentemente sujeitos ? carregamentos c?clicos e condi??es ambientais de temperatura e umidade, que podem provocar degrada??o e at? a falha do componente. O objetivo deste trabalho foi estudar os efeitos do envelhecimento sob exposi??o a temperatura at? 160?C e ? umidade nos mecanismos de dano de comp?sitos carbono/ep?xi submetidos a carregamento c?clico. Um estudo preliminar de envelhecimento acelerado foi inicialmente realizado em comp?sitos unidirecionais AS4/8552 com ciclo exposi??o de 8 h de radia??o UVA-340 a 80?C seguidas de 4 h de condensa??o a 50?C, at? atingir o tempo total de 2.160 h. Os efeitos do envelhecimento do material foram evidenciados pela perda de massa, exposi??o das fibras, altera??es qu?micas, aumento da densidade de trincas em testes de cisalhamento interlaminar e flambagem das fibras em amostras fraturadas em testes de compress?o, embora n?o tenham sido observadas altera??es significativas nas propriedades mec?nicas do material. Com base neste trabalho preliminar, um estudo foi realizado em laminados [02/902]s do mesmo material, utilizando ciclo de exposi??o de 8 h a 160 ?C seguidas de 4 h com umidade relativa de 80% a 70 ?C, at? atingir o tempo total de 2.880 h. Em seguida, as amostras foram submetidas a ensaios de fadiga com controle de carga, com raz?o de tens?es R = 0,1 e frequ?ncia de 5 Hz. Os comp?sitos foram caracterizados por espectroscopia de infravermelho com transformada de Fourier (FTIR), an?lise din?mico mec?nica (DMA), microscopia eletr?nica de varredura (MEV) e varia??o de massa, antes e ap?s a exposi??o higrot?rmica. Amostras de ep?xi puro 8552 foram tamb?m expostas as mesmas condi??es de envelhecimento e caracterizadas por microscopia ?tica (MO), espectroscopia FTIR e varia??o de massa. A partir dos diagramas de vida em fadiga, uma fun??o de deslocamento (shift) foi proposta para a previs?o de n?mero de ciclos para falha de comp?sitos envelhecidos com base em dados de testes de fadiga em comp?sitos n?o envelhecidos. O estudo tamb?m mostrou que a falha por fratura pode n?o ser o melhor par?metro para avalia??o do efeito do envelhecimento higrot?rmico na vida em fadiga de materiais comp?sitos de matriz polim?rica refor?ados com fibras de carbono. Outros par?metros como delamina??o e satura??o de trincas s?o tamb?m essenciais para avaliar a durabilidade desses materiais comp?sitos. / Carbon fiber reinforced polymer (CFRP) composites used in aeronautic and aerospace structures are often exposed to cyclic loading and environmental effects such as temperature and humidity, which can lead to degradation and failure of the component. The objective of this work was to study the effects of aging under exposure to temperature up to 160?C and humidity on the damage mechanisms of carbon/epoxy composites subjected to cyclic loading. Initially, a preliminary accelerated aging study was conducted with unidirectional AS4/8552 samples using an exposure cycle of 8 h of UVA-340 at 80 ?C followed by 4 h of condensation at 80 ?C, for a total exposure period of 2,160 h. The effects of aging were evidenced by weight loss, fiber exposure, chemical changes, increased crack density in interlaminar shear strength tests, and fiber buckling in fractured samples after compression tests, even though no significant changes mechanical properties were observed. Based on this preliminary work, a study was conducted on [02/902]s laminates of the same material, using an exposure cycle of 8 h at 160 ?C followed by 4 h of 80% relative humidity at 70 ?C, for a total exposure period of 2,880 h. Afterwards, stress-controlled tension-tension fatigue tests were conducted using a stress ratio R = 0.1 and frequency of 5 Hz. Composites were characterized using Fourier transform infrared spectroscopy (FTIR), Dynamic Mechanical Analysis (DMA), Scanning Electron Microscopy (SEM) and weight change, before and after hygrothermal exposure. Samples of plain epoxy 8552 were also exposed to the same aging conditions and characterized by optical microscopy (OM), FTIR spectroscopy and weight change. Based on the fatigue life diagrams, a shift function was proposed for the prediction of number of cycles to failure of aged composites based on data from unaged specimens. The study also showed that failure by fracture may not be the best parameter to evaluate the effect of hygrothermal aging on fatigue life of carbon fiber reinforced polymer composites. Other parameters such as delamination and crack saturation are also essential to assess durability of these composites.
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Caracteriza??o de comp?sito ep?xi/tecido de pet p?s-consumoRibeiro, Fernanda Alves 11 October 2016 (has links)
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Previous issue date: 2016-10-11 / O consumo esmagador de Polietileno tereftalado (PET) grau garrafa constitui cap?tulo ? parte
entre as resinas produzidas no Brasil. Embora o pa?s consiga reciclar mais da metade da
produ??o de PET, ainda ? muito elevado o volume deste material em forma de garrafas.
Salienta-se que, apesar do benef?cio da resina PET poder ser utilizada em in?meras aplica??es
e sob diversos processos, ? necess?rio desenvolver alternativas de seu reuso na via de
reciclagem. Nesta vertente, o objetivo da pesquisa foi avaliar a aplica??o do tecido de pet,
oriundo do processo de reciclagem das garrafas, como refor?o de comp?sitos polim?ricos.
Para tanto, na metodologia utilizada, ap?s a preliminar caracteriza??o do tecido de pet via
ensaios t?xteis (Determina??o de gramatura; Resist?ncia ? propaga??o ao rasgo; Resist?ncia ?
tra??o e alongamento), confeccionou-se laminados comp?sitos polim?ricos com matriz ep?xi
e diferentes fra??es de tecido para a verifica??o e an?lise de suas principais propriedades
f?sico-qu?micas, mec?nicas e t?rmicas. Os seguintes ensaios foram realizados nos corpos de
prova de resina e laminado comp?sito: Densidade; Absor??o de ?gua; Teor de umidade;
Tra??o uniaxial; Flex?o em tr?s pontos; Compress?o; Dureza; TG; DMA e An?lise de fratura.
A an?lise dos resultados evidenciou que o incremento de camadas de tecido propicia ao
comp?sito o aumento nas resist?ncias ? tra??o e ? compress?o; al?m do que, eleva a rigidez
viscoel?stica do material, ao passo que diminui a resist?ncia ? flex?o. Observou-se tamb?m
que as camadas de tecido de PET diminuem o teor de umidade do comp?sito, bem como a sua
capacidade de absor??o de ?gua. Contudo, as propriedades Dureza e Densidade n?o
apresentaram varia??o significativa com a inclus?o do tecido de PET. A configura??o P90,
com o m?ximo teor de tecido de PET no laminado, exprimiu-se como a de melhor
desempenho frente aos ensaios realizados. Deste modo, a utiliza??o do tecido PET evidencia
aspectos atraentes para as iniciativas empresariais do setor. A composi??o P90, como refor?o
de comp?sito polim?rico, foi a que apresentou melhor resultado. Esse material tr?s reflexos
socio-econ?micos diretamente relacionados com a melhoria da qualidade de vida da
popula??o, gera??o de renda, economia de recursos naturais e atenua??o de problemas
ambientais. / There is no doubt whatsoever that the widest consumption of polyethylene terephthalate
(PET) bottle grade is a unique chapter among the resins produced in Brazil. Although the
country is able to recycle more than a half of all PET production, the number of such material
for bottle fabrication is still very high. It is important to remark that, though all benefits of
PET resin uses in uncountable applications and under many processes; alternatives to its reuse
throughout recycling dynamics must be developed. Thus, this work aims at evaluating the
application of PET fabric coming from the process of bottle recycling polymeric composite
reinforcements. In order to do so, after a preliminary characterization of the PET fabric by
textile tests (Grammage determination; Tear propagation resistance; Tensile strength and
elongation resistance), laminated polymeric composite with epoxy matrix as well as different
fractions of fabric for checking and analysis of their main physicochemical, mechanical and
thermal properties were engendered. The following tests were performed with the resin and
with laminated composite: Density, Water absorption; Moisture content; Uniaxial tensile;
Three point flexural test; Compression; Hardness; TG; DMA and Fracture analysis. By
analyzing the results, it was noticed that the increase of fabric layers provide a resistance and
compression gain to the composite, and it also increases the material viscoelastic stiffness, at
the same time as its flexural strength is diminish. It was also noticed that its water absorption
capacity was diminished. Nevertheless, its hardness and density properties did not present
meaningful variation with the PET addition. The P90 setting with the highest content of PET
fabric in the laminate presented itself as having the best results in the tests. Therefore the use
of PET fabric presents attracting aspects to entrepreneurship. P90 configuration used as
polymeric composite reinforcements were the one to present the best results. Such material
brings socio-economical reflexions directly linked to the improvement of livelihood, natural
resources economy and offset environment problems.
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Desenvolvimento de comp?sito um de matriz polim?rica com carga/refor?o de fibras de pia?ava e pet p?s-consumoLima, Rudson de Souza 05 June 2017 (has links)
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Previous issue date: 2017-06-05 / Diante da realidade mundial de preserva??o ambiental, da necessidade de reaproveitamento de insumos, redu??o de custos e melhoramento de propriedades, tem-se desenvolvido muitas tecnologias que atendam a uma s?rie desses fatores e, se poss?vel, a todos. Nesse sentido, os materiais comp?sitos assumem um papel de destaque nesse desenvolvimento de novos materiais. O PET (Polietileno tereftalato) tem sido muito utilizado pela ind?stria mundial em v?rias aplica??es, onde a principal dessas ? a produ??o de embalagens de produtos de aliment?cios, em que as ind?strias de refrigerantes s?o os grandes consumidores desse produto. J? na linha de fibras naturais, existe uma vasta quantidade de op??es de uso em aplica??es de engenharia (Sisal, carna?ba, algod?o, pia?ava, etc.). Diante do exposto, esse trabalho visa ? produ??o, caracteriza??o (Mec?nicos, t?rmicos e f?sicos) e compara??o de uma s?rie de configura??es de materiais comp?sitos com uma matriz polim?rica (Ep?xi) com refor?o de PET p?s-consumo e pia?ava (Resina ep?xi para refer?ncia; ep?xi com fibras de PET; ep?xi com fibras de pia?ava; e comp?sito h?brido). Os comp?sitos foram produzidos com fibras bidirecionais em forma de tecido, as fibras tinham espa?amento entre elas de 1 cm. Os materiais refor?ados promoveram aumento de algumas propriedades, como flex?o, que apresentou um incremento de cerca de 25% na tens?o m?xima admiss?vel do material. Observou-se que a ordena??o das fibras em sentido unidirecional pode melhorar as resist?ncias mec?nicas do comp?sito, isso porque, de forma geral, todas as rupturas dos ensaios ocorreram em uma sec??o de fragiliza??o provocada pelas fibras transversais aos esfor?os. Quando submetidos a esfor?os mec?nicos, o comp?sito com refor?o/carga de PET apresentou-se como a melhor configura??o, o qual apresentou um m?dulo de elasticidade em regime de flex?o 24% maior que a resina pura. J? em an?lise t?rmica, o comp?sito h?brido apresentou melhores caracter?sticas para isolamento t?rmico, visto que sua condutividade t?rmica reduziu em 2% quando comparado com o ep?xi puro. / Over the world reality of environment preservation, the necessity of reuse supplies, reduction of costs and improvement of properties, it has been developed many technologies that support a series of these factors and, if possible all of them. In this sense, the composite materials assume a special role in the growth of new materials. The PET (polyethylene terephthalate) has been utilized by worldwide industries in many different applications, from which the principal one of them is the packaging of food production, wherefrom the soft drink industries are the most substantial consumer of this product. As for natural fibers research line, there is a vast quantity of options for engineering application handling (Sisal, carnauba, cotton, piassava, etc.) In the face of what has been exposed, this research strives for the production, characterization (Mechanical, thermal and physical) and comparison of a series of configurations in the composite materials with a polymer matrix (Epoxy) with reinforcement of PET after consummation and piassava (epoxy resin for reference; enhancement resin with piassava fibers; and hybrid composite). The composites were produced with bidirectional fibers in a format of tissue, the fibers had spaces between them of 1 centimeter. The reinforced materials promoted increment of some properties, such as flection, that presented an enhancement of nearly 25% of maximum tension admitted in the material. It was observed however, that the ordination of the fibers in a unidirectional way might improve the mechanic resistance of the composite, that?s because, in general form, all the ruptures occur in one section of fragilization provoked by the transversal fibers to the reinforces. While submitted to mechanic reinforces, the composite with reinforce/charge of PET presented itself with an improved configuration, Which showed a modulus of elasticity in a regime of flexion 24% larger than the pure resin. As for the thermal analysis, the hybrid composite presented enriched characteristics for the thermal insulation, since its thermal conductivity reduced by 2% when compared to the pure epoxy.
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Efeito da adi??o de grafite expandido por microondas nas propriedades t?rmicas, el?tricas e mec?nicas de nanocomp?sitos de matriz ep?xiMarinho, Ant?nio Calmon de Ara?jo 26 February 2014 (has links)
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Previous issue date: 2014-02-26 / Universidade Federal do Rio Grande do Norte / Epoxy based nanocomposites with 1 wt % and 3 wt % of nanographite were
processed by high shear mixing. The nanographite was obtained by chemical (acid
intercalation), thermal (microwave expansion) and mechanical (ultrasonic exfoliation)
treatments. The mechanical, electrical and thermal behavior of the nanocomposites
was determined and evaluated as a function of the percentage of reinforcement.
According to the experimental results, the electrical conductivity of epoxy was not
altered by the addition of nanographite in the contents evaluated. However, based on
the mechanical tests, nanocomposites with addition of 1 wt.% and 3 wt.% of
nanographite showed increase in tensile strength of 16,62 % and 3,20 %,
respectively, compared to the neat polymer. The smaller increase in mechanical
strength of the nanocomposite with 3 wt.% of nanographite was related to the
formation of agglomerates. The addition of 1 wt.% and 3 wt.% of nanographite also
resulted in a decrease of 6,25 % and 17,60 %, respectively, in the relative density of
the material. Thus, the specific strength of the nanocomposites was approximately
33,33 % greater when compared to the neat polymer. The addition of 1 wt.% and 3
wt.% of nanographite in the material increased the mean values of thermal
conductivity in 28,33 % and 132,62 %, respectively, combined with a reduction of
26,11 % and 49,80 % in volumetric thermal capacity, respectively. In summary, it has
been determined that an addition of nanographite of the order of 1 wt.% and 3 wt.%
produced notable elevations in specific strength and thermal conductivity of epoxy / Nanocomp?sitos a base de resina ep?xi e nanografite foram processados por
mistura de alto cisalhamento, com concentra??es de 1 % e 3 % p/p de refor?o. O
nanografite foi obtido atrav?s de tratamentos: qu?mico (intercala??o ?cida), t?rmico
(expans?o por microondas) e mec?nico (esfolia??o por ultrassom). Os
comportamentos mec?nico, el?trico e t?rmico dos materiais obtidos foram analisados
em fun??o da porcentagem de refor?o. De acordo com os resultados obtidos, n?o
foram verificadas altera??es na condutividade el?trica do ep?xi com a adi??o de
nanografite, nos percentuais estudados. Entretanto, com base nos ensaios
mec?nicos observou-se que os nanocomp?sitos com adi??o de 1 % p/p e 3 % p/p de
grafite expandido apresentaram aumento na resist?ncia ? tra??o de 16,62 % e 3,20
% respectivamente, em rela??o ao pol?mero puro. O menor aumento de resist?ncia
mec?nica para os nanocomp?sitos com 3 % p/p de nanografite foi relacionado com a
forma??o de aglomerados. A adi??o de 1 % p/p e 3% p/p de nanografite tamb?m
resultou em uma diminui??o de 6,25 % e 17,60 %, respectivamente, na densidade
relativa do pol?mero. Portanto, a eleva??o da resist?ncia espec?fica dos
nanocomp?sitos foi de aproximadamente 33,33% para os dois nanocomp?sitos, em
rela??o ao pol?mero puro. A adi??o de 1 % p/p e 3 % p/p de nanografite no material
aumentou os valores m?dios de condutividade t?rmica em 28,33 % e 132,62 %,
respectivamente, combinado com uma redu??o de 26,11 % e 49,80 %,
respectivamente, na capacidade t?rmica volum?trica. Em resumo, verificou-se que
uma adi??o de nanografite da ordem de 1 % e 3 % p/p produziram eleva??es
not?veis na resist?ncia mec?nica espec?fica e condutividade t?rmica do ep?xi
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Morfologia e propriedades mec?nicas da fibra de sisal unidirecional e em sobreposi??o de comp?sito com resina ep?xi / Morphology and mechanical properties of the fiber and overlapping unidirectional composite with epoxy resinHolanda, Elis?ngela Bezerra das Neves 14 January 2013 (has links)
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Previous issue date: 2013-01-14 / Coordena??o de Aperfei?oamento de Pessoal de N?vel Superior / The composites manufactured with long fibres aligned in a single direction, and overlay has been shown to have better performance than the short fibers randomly distributed. In particular, the lignocellulosic fibers extracted from the sisal leaves, used in conjunction with the epoxy resin has attracted the attention of many researchers because the final properties of the system formed. In this work composites based on epoxy resin reinforced with sisal fibers were manufactured. The sisal fibres were treated with an alkaline solution of 0.06 mol/l NaOH. The treated, and untreated fibres were subjected to tension x extension tests. The composites were manufactured in the "Lossy" mold with the specifications of the samples to be produced (300x20x4 mm). The tension tests were carried out in accordance with the ASTM standards 3039 (for the composite aligned in a single direction) and ASTM D5573 (for composites in overlay), three point bending tests were performed according to ASTM D790. Analyzing the results of the tests of tension and three point bending tests, it was observed that the composites with the configuration of overlapping had the better elastic module in both tests. As to the maximum resistance to tension, the best result was the composites aligned in a single direction. Tests of absorption of water and micrographs are in progress / Os comp?sitos fabricados com fibras longas alinhadas unidirecionalmente e em sobreposi??o tem demonstrado que possuem melhor desempenho do que as fibras cortadas aleatoriamente distribu?das. Em especial, as fibras lignocelul?sicas extra?das do sisal, utilizadas em conjunto com a resina ep?xi tem atra?do a aten??o de muitos pesquisadores devido ?s propriedades finais do sistema formado. No presente trabalho foram fabricados comp?sitos ? base de resina ep?xi refor?ado com fibras de sisal. As fibras de sisal foram submetidas ao tratamento alcalino com NaOH a 0,06 mol/l, em seguida submetidas ao ensaio de tra??o na fibra tratada e n?o tratada. Os comp?sitos foram fabricados no molde denominado de Lossy (molde com perdas) usinado de acordo com as especifica??es das amostras a serem produzidas (300x20x4 mm). Os ensaios de tra??o foram realizados de acordo com as normas ASTM 3039 (Para os comp?sitos alinhados unidirecionalmente) e ASTM D5573 (Para os comp?sitos em sobreposi??o), os ensaios de flex?o em tr?s pontos foram realizados de acordo com as normas ASTM D 790. Analisando os resultados dos ensaios de tra??o e flex?o em tr?s pontos, foram observados que os comp?sitos com a configura??o de sobreposi??o teve melhor m?dulo de elasticidade em ambos os ensaios. Quanto a resist?ncia m?xima a tra??o o melhor resultado foi do comp?sito alinhado unidirecionalmente. No ensaio de absor??o de ?gua foi observado que os comp?sitos possuem um n?vel muito baixo de absor??o e o comp?sito alinhado unidirecionalmente obteve percentual de satura??o de 1,97 %. Nas micrografias, se observa as regi?es de ruptura/trincas do comp?sito e seu comportamento (fibra/matriz)
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Adi??o de poli(etileno-co-?cido-metacr?lico) (EMAA) como agente de auto-reparo em comp?sitos carbono-ep?xiNascimento, Allana Azevedo do 16 October 2017 (has links)
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Previous issue date: 2017-10-16 / As t?cnicas de auto-reparo em resinas ep?xi v?m sendo desenvolvidas buscando aumentar a vida ?til e reduzir os custos associados ? manuten??o desses materiais durante o servi?o. A adi??o de termopl?sticos ? matriz termofixa produzindo resinas repar?veis aparece como t?cnica de reparo promissora. Neste trabalho, o termopl?stico poli (etileno-co-?cido-metacr?lico) (EMAA) foi adicionado no plano m?dio de laminados comp?sitos carbono-ep?xi para fabrica??o de um sistema de reparo. Foram fabricadas placas com 5%, 10% e 15% de EMAA em massa de resina do prepreg. Ensaios de resist?ncia ao cisalhamento interlaminar (ILSS), an?lise din?mico mec?nica (DMA), espectroscopia de infravermelho por transformada de Fourier (FTIR), microscopia eletr?nica de varredura (MEV) e microscopia eletr?nica de varredura com fonte de emiss?o de campo (MEV-FEG) foram conduzidos para avaliar o efeito da adi??o desse termopl?stico ao comp?sito e seu comportamento antes e ap?s o reparo. As amostras reparadas n?o apresentaram aumento na resist?ncia ao cisalhamento interlaminar (ILSS) ap?s o reparo. Entretanto, para maiores porcentagens de EMAA, houve redu??o dessa propriedade, al?m de redu??o de m?dulo de elasticidade e da temperatura de transi??o v?trea (Tg), em rela??o aos valores apresentados pelo comp?sito puro. Imagens de MEV confirmaram a forte ades?o entre o EMAA e a resina ep?xi, formando uma camada adesiva que impediu a forma??o de delamina??es no plano m?dio do laminado. / Self-healing techniques in epoxy resins have been developed to improve the durability and reduce costs associated with repairs of these materials during service. The addition of thermoplastics into the thermoset matrix producing mendable resins appears as a promising self-healing technique. In this study, poly(ethylene-co-methacrylic acid) (EMAA) was added in the mid-plane of carbon fiber-epoxy composites laminates to produce a self-healing system. Plates were manufactured with addition of 5%, 10% and 15% of EMAA as related to the resin weight of prepreg. Interlaminar shear strength test (ILSS), dynamic mechanical analysis (DMA), Fourier-transform infrared (FTIR) spectroscopy, scanning electron microscopy (SEM) and field-emission gun scanning electron microcopy (FEG-SEM) were employed in order to evaluate the effect of the addition of the thermoplastic to the composite and its behavior before and after a healing cycle. The healed samples did not show an increase in interlaminar shear strength (ILSS) after healing. However, for higher percentages of EMAA there was a reduction of this property, besides a reduction of Young?s modulus and glass transition temperature (Tg), in relation to the values presented by the unmodified composite. SEM images confirmed the strong adhesion between EMAA and epoxy resin, which produced an adhesive layer that prevented delamination in the mid-plane of the laminate.
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Influ?ncia da sequ?ncia de empilhamento nas propriedades mec?nicas de laminados comp?sitos submetidos ? tra??oFernandes, Pedro Lucas Serafim 21 July 2014 (has links)
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Previous issue date: 2014-07-21 / Conselho Nacional de Desenvolvimento Cient?fico e Tecnol?gico / Composite laminates with plies in different directions finely dispersed are classified as homogenized. The expected benefits of homogenization include increased mechanical strength, toughness and resistance to delamination. The objective of this study was to evaluate the effect of stacking sequence on the tensile strength of laminates. Composite plates were fabricated using unidirectional layers of carbon/epoxy prepreg with configurations [903/303/-303]S and [90/30/-30]3S. Specimens were subjected to tensile and open hole tension (OHT) tests. According to the experimental results, the mean values of strength for the homogenized laminates [90/30/-30]3S were 140% and 120% greater for tensile and OHT tests, respectively, as compared to laminates with configuration [903/303/-303]S. The increase in tensile strength for more homogenized laminates was associated with the increment in interlaminar interfaces, which requires more energy to produce delamination, and the more complicated crack propagation through plies with different orientations. OHT strength was not affected by the presence of the hole due to the predominance of the interlaminar shear stress in relation to the stress concentration produced by the hole / Laminados formados por l?minas com diferentes orienta??es, finamente dispersas, s?o classificados como homogeneizados. Os benef?cios esperados da homogeneiza??o incluem aumento de resist?ncia mec?nica, da tenacidade e da resist?ncia ? delamina??o. O objetivo deste trabalho foi avaliar o efeito da sequ?ncia de empilhamento na resist?ncia ? tra??o de laminados quase-isotr?picos. Placas de comp?sitos foram fabricadas com l?minas unidirecionais de ep?xi/carbono com configura??es [903/303/-303]S e [90/30/-30]3S. Corpos de prova foram submetidos a ensaios de tra??o e de open hole tension (OHT). De acordo com os resultados experimentais, os valores m?dios de resist?ncia para os laminados mais homogeneizados [90/30/-30]3S foram incrementados em 140% e 120% nos ensaios de resist?ncia ? tra??o e OHT, respectivamente, em rela??o aos laminados com configura??o [903/303/-303]S. O aumento de resist?ncia ? tra??o para laminados mais homogeneizados foi relacionado com o maior n?mero de interfaces interlaminares, que aumenta a quantidade de energia necess?ria para produzir delamina??o, e a maior dificuldade de propaga??o de trincas atrav?s de l?minas com orienta??es diferentes. A resist?ncia medida nos ensaios de OHT n?o foi afetada pela presen?a do furo devido ? predomin?ncia da influ?ncia da tens?o de cisalhamento interlaminar em rela??o ao efeito de concentra??o de tens?o provocado pelo furo
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