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Influence of Angle Ply Orientation on the Flexural Strength of Basalt and Carbon Fiber Reinforced Hybrid Composites

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초록

In this paper the influence of fiber orientation of basalt and carbon inter-ply fabrics on the flexuralproperties of hybrid composite laminates was experimentally investigated. Four types of basalt/carbon/epoxy inter-plyhybrid composite laminates with varying angle ply orientation of reinforced basalt fiber and fixed orientation ofcarbon fiber were fabricated using hand lay-up technique. Three point bending test was performed according toASTM 7264. The fracture surface analysis was carried out by scanning electron microscope (SEM). The resultsobtained from the four laminates were compared. Lay-up pattern of [0B/+30B/-30B/0C]S exhibits the best propertiesin terms of flexural strength and flexural modulus. Scanning electron microscopy results on the fracture surfaceshowed that the interfacial de-bonding between the fibers and epoxy resin is a dominant fracture mode for all fiberlay-up schemes.

Abstract

In this paper the influence of fiber orientation of basalt and carbon inter-ply fabrics on the flexuralproperties of hybrid composite laminates was experimentally investigated. Four types of basalt/carbon/epoxy inter-plyhybrid composite laminates with varying angle ply orientation of reinforced basalt fiber and fixed orientation ofcarbon fiber were fabricated using hand lay-up technique. Three point bending test was performed according toASTM 7264. The fracture surface analysis was carried out by scanning electron microscope (SEM). The resultsobtained from the four laminates were compared. Lay-up pattern of [0B/+30B/-30B/0C]S exhibits the best propertiesin terms of flexural strength and flexural modulus. Scanning electron microscopy results on the fracture surfaceshowed that the interfacial de-bonding between the fibers and epoxy resin is a dominant fracture mode for all fiberlay-up schemes.

참고문헌 (11)

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  8. Faulstich de Paiva, J. M, "Mechanical and Morphological Characterizations of Carbon Fiber Fabric Reinforced Epoxy Composites used in Aeronautical Field", Journal of Materials Research, 12(3), pp.367~374 (2009)
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