Two-stage hybrid optimization of topology and infill density in polymer extrusion additive manufacturing for lightweight high-integrity structures

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Rane, Kedarnath and Bjonnes, Andrew and Walker, Dickon and Seth, Sampan (2025) Two-stage hybrid optimization of topology and infill density in polymer extrusion additive manufacturing for lightweight high-integrity structures. Applied Sciences, 15 (22). 12258. ISSN 2076-3417 (https://doi.org/10.3390/app152212258)

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Abstract

Material Extrusion (MEX) additive manufacturing offers a versatile platform for producing lightweight, structurally optimized components. This study investigates the simultaneous optimization of topology and infill density using three polymer composite materials, PPA-CF, PAHT-CF, and ABS, selected for their mechanical performance, cost efficiency, and printability. Cylindrical specimens were fabricated with nine mass retention levels (100% to 33%) by systematically varying topology and infill parameters. Compression testing was conducted to assess stiffness, deformation behavior, and structural integrity under simulated operational loads. Results show that combining topology optimization with variable infill density can significantly reduce material usage and manufacturing time while maintaining mechanical reliability across all three materials. PAHT-CF demonstrated the highest strength-to-weight performance, while ABS offered cost-effective alternatives for less demanding applications. The study establishes clear relationships between design strategies and material behavior, enabling the production of net-shape satellite support structures with fewer design iterations and improved throughput. These findings support the adoption of resource-efficient manufacturing practices and provide a framework for sustainable, low- to mid-volume production in high-value manufacturing industries. Overall, the integration of design and material optimization advances the potential of additive manufacturing for scalable, cost-effective, and environmentally conscious aerospace solutions.

ORCID iDs

Rane, Kedarnath ORCID logoORCID: https://orcid.org/0000-0002-9405-7950, Bjonnes, Andrew, Walker, Dickon ORCID logoORCID: https://orcid.org/0009-0009-2071-2105 and Seth, Sampan ORCID logoORCID: https://orcid.org/0000-0002-2563-4574;
CORE (COnnecting REpositories)