The influence of processing method on the fracture toughness of thermoplastic-modified, carbon-fiber-reinforced epoxy composites has been investigated. The composites used in this work were prepared from toughened epoxy (176°C cure) prepregs with carbon fiber reinforcement. Tetraglycidyl-4,4 ′-diaminodiphenyl methane (TGDDM) type epoxy resin was used as a matrix material and the polyacrylonitrile based T-300 (12 K) type was used as a carbon fiber. The prepregs had 37 wt.% of resin and a fiber areal weight of 145 ± 3 g/m 2. Poly(butylene terephthalate) (PBT) was used as a dispersed phase. Nylon 6 was also tried as a dispersed phase. In order to optimize the preparation and the toughness of the prepreg, three different processes were attempted; spray-up, double pass, and general types. The mode-II interlaminar fracture toughness was determined in terms of G IIc by using the end-notch-flexure (ENF) test. The toughness of the composite was investigated as a function of the prepreg preparation method, resin formulation, and the kinds and contents of a dispersed phase. It was found that the double-pass impregnation produces composites with higher toughness, compared with the general type of preparation process. Prepregs with an epoxy formulation with lower TGDDM content exhibited higher toughness. The prepregs toughened with Nylon 6 always showed higher G IIC, glass-transition temperatures, as compared with those with PBT, regardless of the preparation methods and the formulation. Finally, it was concluded that the toughness of composites made from prepreg prepared by the spray-up preparation method shows a maximum when the PBT content was 15 phr.
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