Characterization of cure of carbon/epoxy prepreg used in aerospace field
Carbon/epoxy 8552 prepreg is a thermoplastic toughened high-performance epoxy being used in the manufacture of advanced army material. Understanding the cure behavior of a thermosetting system is essential in the development and optimization of composite fabrication processes. The cure kinetics and...
| Autores: | ; ; ; |
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| Tipo de documento: | Artículo |
| Estado: | Published version |
| Fecha de publicación: | 2005 |
| País: | Brasil |
| Institución: | UNESP |
| Repositorio: | Repositório Institucional da UNESP |
| Lenguaje: | Inglés |
| OAI Identifier: | oai:repositorio.unesp.br:11449/68310 |
| Acceso en línea: | http://dx.doi.org/10.1590/S1516-14392005000300016 http://hdl.handle.net/11449/68310 |
| Nivel de acceso: | Acceso abierto |
| Palabra clave: | Carbon/epoxy prepreg DMA DSC Kinetic of cure Rheology Aerospace engineering Carbon Curing Differential scanning calorimetry Dynamic mechanical analysis Mathematical models Optimization Rheometers Thermal effects Thermosets Carbon/epoxy prepegs Thermosetting systems Epoxy resins |
| Sumario: | Carbon/epoxy 8552 prepreg is a thermoplastic toughened high-performance epoxy being used in the manufacture of advanced army material. Understanding the cure behavior of a thermosetting system is essential in the development and optimization of composite fabrication processes. The cure kinetics and rheological behavior were evaluated using a differential scanning calorimetry (DSC), dynamic mechanical analysis (DMA) and a rheometer. Values of the kinetic parameters were obtained from dynamic DSC scans using an nth order reaction model. Rheological measurements as a function of temperature and time were made for the prepreg system. The manufacturer's recommended cure cycle was evaluated and considered adequate to consolidated the studied system. |
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