The Effects of Manufacturing Techniques on the Mechanical Performance of an Auxetic Structure Manufactured by Fused Filament Fabrication and Multijet Fusion Processes

Abstract

Additive manufacturing is increasingly becoming potential for short‐run part production. The aim of this work is to explore the mechanical properties of a hybrid auxetic structure fabricated by multijet fusion (MJF) and fused filament fabrication (FFF). The experimental measurements indicate that robust specimens with high‐dimensional accuracy are successfully achieved using MJF process. In the case of the FFF process, the walls–walls and walls–cylinders areas (connecting areas) suffer large pores, indicating poor printing quality. The 3D printed specimens via FFF process reveal smooth plateau stress, while plateau stress with high peaks is observed when the MJF specimens are compressed along the Y‐axis. Moreover, specimens manufactured by the MJF process reveal the highest specific energy absorption (SEA) per unit volume and per unit mass. The calculated values of SEA are 2.1 and 2.5 J g−1 (for specimens fabricated by MJF) in which they significantly outperform the SEA (0.495 and 0.480 J g−1) of those manufactured by the FFF process. Furthermore, the trend of auxetic features (negative Poisson's ratio) has not been affected by the manufacturing processes. This study sheds light on the influence of fabrication methods on the mechanical properties of cellular materials especially their ability to absorb energy.

Experimental investigations into 3D printed hybrid auxetic structures for load-bearing and energy absorption applications

“…Moreover, AM route is economically sustainable due to design freedom, simplification in part fixturing, and proper utilization of feedstock materials [25]. FFF [26,27], MJF [28,29], FDM [30,31], SLA [32,33], SLS [34,35], and SLM [36,37], etc. are widely used for the fabrication of vibrational energy harvester, vessel stent [38], lightweight auxetic frames for smart sensors [39], vascular scaffolds [40], star-rhombic honeycomb structure for explosion proof containers and fuselages of the aerial vehicles [41,42].…”