Investigates how nozzle diameter and infill patterns affect mechanical strength in composite structures, suggesting optimal designs for lightweight applications.
This study systematically investigated the synergistic effects of nozzle diameter and infill geometry on the mechanical properties and lightweight potential of short carbon fiber-reinforced ABS composites fabricated by fused deposition modeling (FDM). Sandwich specimens were produced with three nozzle diameters (0.4, 0.6, and 0.8 mm) and four infill patterns: Gyroid, 2D-honeycomb, 3D-honeycomb, and solid. Three-point flexural tests revealed that increasing the nozzle diameter from 0.4 mm to 0.8 mm significantly enhanced interlayer bonding, leading to a maximum improvement of 21.7% in flexural strength (Gyroid) and 25.3% in flexural modulus (solid infill). At 50% infill density, the 3D-honeycomb structure exhibited superior performance, with 4.7%-19.5% higher flexural strength and 2.89%-20.4% higher modulus than other infill types. Notably, the mass-normalized analysis highlighted the Gyroid structure as the most efficient in material utilization. With a 0.8 mm nozzle system, the strength could reach 14.11 MPa/g and the modulus could reach 574.24 MPa/g, highlighting its unique lightweight potential. Microscopic crack observations further elucidated the distinct failure mechanisms governed by the interplay between nozzle diameter and infill architecture. This work provided a comprehensive understanding of the process-structure-performance relationship in FDM-fabricated composites, offering practical guidelines for parameter selection in automotive lightweight applications.
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Wang et al. (2026) studied this question.
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