TY - JOUR
T1 - Polymer micro-lattice buffer structure free impact absorption
AU - Catar, Louis
AU - Tabiai, Ilyass
AU - St-Onge, David
N1 - Publisher Copyright:
© IMechE 2026. This article is distributed under the terms of the Creative Commons Attribution 4.0 License (https://creativecommons.org/licenses/by/4.0/) which permits any use, reproduction and distribution of the work without further permission provided the original work is attributed as specified on the SAGE and Open Access page (https://us.sagepub.com/en-us/nam/open-access-at-sage).
PY - 2026
Y1 - 2026
N2 - Advances in miniaturized electronics, perception modules, and flight controllers have expanded the use of uncrewed aerial systems (UAS) to indoor applications such as warehouse management, inspection, and subterranean exploration. Yet, no safety standards currently address the risks of lightweight aerial vehicles operating near humans. This study investigates ultra-light micro-lattice structures as protective elements to enhance crashworthiness without significantly affecting flight endurance. Patch samples with Face-Centered Cubic (FCC), Diamond (D), Kelvin (K), and Gyroid (GY) patterns were fabricated at an effective density of 65 kg/m3 and tested under compression and impact loading. Results show that Diamond and Kelvin lattices distribute loads more efficiently, achieving specific energy absorption values above 1000 J/kg, while impact tests reveal that flexible patches dissipate energy more effectively and maintain integrity under dynamic loading compared to rigid designs.
AB - Advances in miniaturized electronics, perception modules, and flight controllers have expanded the use of uncrewed aerial systems (UAS) to indoor applications such as warehouse management, inspection, and subterranean exploration. Yet, no safety standards currently address the risks of lightweight aerial vehicles operating near humans. This study investigates ultra-light micro-lattice structures as protective elements to enhance crashworthiness without significantly affecting flight endurance. Patch samples with Face-Centered Cubic (FCC), Diamond (D), Kelvin (K), and Gyroid (GY) patterns were fabricated at an effective density of 65 kg/m3 and tested under compression and impact loading. Results show that Diamond and Kelvin lattices distribute loads more efficiently, achieving specific energy absorption values above 1000 J/kg, while impact tests reveal that flexible patches dissipate energy more effectively and maintain integrity under dynamic loading compared to rigid designs.
KW - additive manufacturing
KW - impact
KW - micro-lattices
KW - photosensitive polymers
KW - specific energy absorption
KW - ultra-lightweight structures
UR - https://www.scopus.com/pages/publications/105035237436
U2 - 10.1177/09544062261430975
DO - 10.1177/09544062261430975
M3 - Journal Article
AN - SCOPUS:105035237436
SN - 0954-4062
JO - Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science
JF - Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science
ER -