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Abstract

In this work, the manufacturing technology for an aileron rib for a civil aircraft with advanced CF/PEI thermoplastic composite materials was investigated. In particular, the compression molding method was applied and continuous-carbon-fiber fabric-reinforced polyetherimide (PEI) composite materials were used. The study was focused on the optimization of processing conditions which led to the production of highquality aileron ribs with CF/PEI thermoplastic composites. The design of processing molds and the relationships among the processing conditions, microstructures and mechanical properties (flexural stiffness and strength) of the produced composite parts were presented. The sample quality in relation to processing conditions was evaluated by C-scan, microscopic examination, void content measurement, and mechanical test programs.

Keywords

thermoplastic composite polyetherimide manufacturing compression molding CF/PEI aileron rib

References

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Manufacturing of an Aileron Rib with Advanced Thermoplastic Composites

Abstract

Keywords

References