Abstract

Honeycomb sandwich panels of several cell geometries were created by stretching polycarbonate melts between opposing platens. Perforations for air ingress through one of the platens were employed to enable and direct the formation of cells within the honeycomb, demonstrating a simple means to produce complicated architectures. Platen temperature, consolidation pressure, and platen movement speeds were each investigated to establish a range of effective process parameters. Honeycomb panels were successfully produced with areal densities of 0.18gcm-2 to 0.42gcm-2 and panel thicknesses ranging from 6mm to 32mm. The cell geometries were found to be effectively modeled by Voronoi diagrams seeded by the perforations used for air ingress. This model was validated by the successful production of hexagonal-, square-, and triangular-celled honeycombs, as well as an architecture combining all three cell shapes. Analysis of several samples via computed tomography provided insight into the internal distribution of material. Out-of-plane compressive testing was used to probe the mechanical performance of the structures. Minimal variation in buckling strength was found between the different honeycomb geometries, but post-failure behavior was dependent on cell shape.

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