Influence of Fillers in Stiffener Core and Structural Parameters on Compaction of T-Stiffened Skins in Autoclave Process
Source abstract
Abstract
Using carbon fibre/bismaleimide unidirectional prepregs, T-stiffened skins were fabricated by integral moulding technology of co-bonding in autoclave. The research was focused on comparing the effects of different filler content and structural parameters (curvature and ply sequence considered) on the compaction of T-stiffened skins. The measurement thickness and observation of micrographs were used to characterise the consolidation and compaction of T-stiffeners, and the experimental results indicated that filler content and structural parameters were both significant factors. A non-uniform thickness distribution and thickening at the corner section of T-stiffeners were observed. For T-stiffeners with quasi-isotropic lay-up, more uniform thickness distribution was obtained under the conditions of rolling unidirectional prepregs as fillers into stiffener core and increasing curvature radius, which could help to compact T-stiffeners and eliminate rich resin defect. The results provided in this study will contribute to understanding of the fracture mechanism of T-stiffened skins.
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Research context
OpenAlex topics: Epoxy Resin Curing Processes · Injection Molding Process and Properties · Mechanical Behavior of Composites
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
Affiliations
Key Laboratory of Aerospace Materials and Performance (Ministry of Education), School of Materials Science, and Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China
Beijing Aeronautical Manufacturing Technology Research Institute, Beijing 100024, PR China
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