Detalhes bibliográficos
| Ano de defesa: |
2014 |
| Autor(a) principal: |
Barbosa, Fernando Montanare [UNESP] |
| Orientador(a): |
Não Informado pela instituição |
| Banca de defesa: |
Não Informado pela instituição |
| Tipo de documento: |
Tese
|
| Tipo de acesso: |
Acesso aberto |
| Idioma: |
por |
| Instituição de defesa: |
Universidade Estadual Paulista (Unesp)
|
| Programa de Pós-Graduação: |
Não Informado pela instituição
|
| Departamento: |
Não Informado pela instituição
|
| País: |
Não Informado pela instituição
|
| Palavras-chave em Português: |
|
| Link de acesso: |
http://hdl.handle.net/11449/111126
|
Resumo: |
This research evaluated the mechanical and thermal properties of composite materials with the base epoxy resin cured (DGEBA / TETA) with the addition of cyclodextrin and reinforced with fibers of bagasse cane sugar. First the fibers were separated into sizes of between 0.50 mm and 2.00 mm, between 0.21 mm and 0.50 mm and smaller than 0.21 mm, which were mixed resin DGEBA / TETA and analyzed as percentages 1, 2.5, 5, 7.5, 10 and 15% in mass by assaying tensile test. Thereafter was added just cyclodextrin epoxy resin in concentrations of 1, 2, 3, 4, 5 and 10 to 15% in mass to analyze tensile test. The specimen of the composite end DGEBA / TETA / cyclodextrin / bagasse fiber cane sugar that is made up of 5% cyclodextrin and 5% of particles smaller than 0.21 mm that was what got the best properties evaluated in separate mechanical tests. Since for the addition of 5% of particles smaller than 0.21 mm at DGEBA / TETA an increase of 28.61% in the resistance, and the addition of cyclodextrin to 5% DGEBA / TETA provided an increase of 160.31% resistance to crack toughness. The final composite, containing 5% of particles of crushed cane sugar and 5% cyclodextrin showed LRT of 33.94 MPa, E, 1681.14 MPa, K1C of 1.24 MPa.m1/2, resilience 0.334 MJ/m3, deformation of 0.292%. For a review of the use temperature of the composite thermal DSC and TGA tests which indicated that the glass transition temperature of the final composite was 111.18 ° C and the onset temperature of degradation was 267°C were performed |
