Abstract

3D woven materials are extremely capable for high-performance aerospace applications. Traditionally, components comprised of 3D wovens are manufactured using Resin Transfer Moulding, requiring matched tooling that can result in high costs. Increasingly this is not feasible for mid-to-large structures, therefore flexible tooling strategies are necessary to facilitate low-cost one-shot vacuum mouldings of multi-textile composites. Towards this need, the authors investigated tooling materials and infusion strategies for an as-designed 3D woven pi-section incorporating a Non-Crimp Fabric (NCF) skin. Engaging with stakeholders presented two infusion strategies (flow ‘up’ or ‘down’ pi-NCF geometry) and three inserts (Polyetherimide, Silicone, and Aluminium) for the pi internal channel. Six infusions were completed with manufacturing data recorded followed by X-ray CT analysis to evaluate geometry and infusion quality; and manufacturing costs estimated. In combination, results suggest that coupling flexible tooling materials is most effective in both reducing costs and maximising injection quality, ensuring geometrical performance.

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