# Structural Analysis and Mechanical Performance of Industrial Conveyor Flight Bars Manufactured with Epoxy Matrix Composites Reinforced by Glass, Carbon, and Kevlar Fibers

**Authors:** Antonio Henrique da Silva Bitencourt Junior, Maurício Maia Ribeiro, Douglas Santos Silva, Raí Felipe Pereira Junio, Sergio Neves Monteiro, Jean da Silva Rodrigues

PMC · DOI: 10.3390/polym18040433 · Polymers · 2026-02-09

## TL;DR

This paper explores using lightweight composite materials as alternatives to steel in conveyor systems, showing significant energy savings and structural safety.

## Contribution

The study introduces a multiscale analytical approach to evaluate composite materials for industrial conveyor flight bars.

## Key findings

- Carbon/epoxy laminates show the lowest longitudinal stresses, indicating superior mechanical performance.
- Replacing steel flight bars with composites reduces moving mass by 82–85%, leading to substantial energy savings.
- Polymer-matrix composites are found to be structurally safe and energetically advantageous for industrial use.

## Abstract

Industrial conveyor systems commonly use steel flight bars, which can account for nearly 50% of the total system mass and significantly affect energy consumption. This study investigates epoxy matrix composites reinforced with glass, carbon, and Kevlar fibers as lightweight alternatives to steel flight bars. A multiscale analytical approach combining micromechanics, Classical Laminate Theory (CLT), and ply-level failure criteria is applied to evaluate the structural response under an industrial bending moment of 342.02 N·m. Tensile tests on vacuum-infused woven glass/epoxy laminates are used to validate micromechanical assumptions and calibrate elastic properties. Ply-wise analysis shows that carbon/epoxy laminates exhibit the lowest longitudinal stresses (≈43 MPa), followed by Kevlar/epoxy (≈53 MPa) and glass/epoxy (≈95 MPa), all well below their respective strength limits. Replacing steel flight bars (4.64 t) with composite alternatives reduces the moving mass to 0.68–0.82 t, corresponding to an 82–85% reduction. This mass reduction significantly lowers the required mechanical power, resulting in an estimated annual energy saving of R$ 8812.80 under continuous operation. Overall, the results demonstrate that polymer-matrix composite flight bars are structurally safe and energetically advantageous, with carbon/epoxy providing the highest mechanical efficiency.

## Full-text entities

- **Genes:** VIP (vasoactive intestinal peptide) [NCBI Gene 7432] {aka PHM27}
- **Diseases:** CLT (MESH:D020240), Fatigue (MESH:D005221), ATH (MESH:D000070896), injury to (MESH:D014947), fracture (MESH:D050723)
- **Chemicals:** hydrogen (MESH:D006859), Epoxy (MESH:D004853), Glass/Epoxy Laminate (-), aluminum (MESH:D000535), silica (MESH:D012822), E (MESH:D004540), Carbon (MESH:D002244), polymer (MESH:D011108), steel (MESH:D013232)
- **Species:** Homo sapiens (human, species) [taxon 9606]
- **Cell lines:** 14574 — Homo sapiens (Human), Transformed cell line (CVCL_1L12)

## Full text

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## Figures

14 figures with captions in the complete paper: https://tomesphere.com/paper/PMC12944644/full.md

## References

32 references — full list in the complete paper: https://tomesphere.com/paper/PMC12944644/full.md

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Source: https://tomesphere.com/paper/PMC12944644