Design of a hybrid carbon fibre/carbon nanotube composite for enhanced lightning strike resistance
Design of a hybrid carbon fibre/carbon nanotube composite for enhanced lightning strike resistance
This work presents a set of analytical design models to predict the electrical and mechanical properties of hybrid carbon nanotubes (CNT)/carbon-fibre (CF)/epoxy composites for potential use in fuselage and airframe constructions against lightning strike. The models are validated by experimental data from open literature. An optimization process is carried out to identify the microstructural configuration of the composite that provides the highest improvement in terms of electrical conductivity for the lowest structural weight in a CFRP fuselage design. The through-the-thickness conductivity of the composite laminate is considerably enhanced by a 2% volume fraction dispersion of CNTs within the matrix resin. The increase in the dielectric properties is accompanied by a moderate improvement of the composite mechanical performance. The hybrid CFRP/CNT composite configuration leads to a weight-efficient design solution for representative fuselage structures.
367-377
Ma, Xiang
e00054e2-db8d-44c6-be6c-7cf807f0f6d3
Scarpa, Fabrizio
684472c3-1a28-478a-a388-5fd896986c1d
Peng, Hua-Xin
4f71af24-3d5b-4edf-ad53-53aa93dab4da
Allegri, Giuliano
8dd43a78-5f53-472f-853a-1b2fd7b129e4
Yuan, Jie
4bcf9ce8-3af4-4009-9cd0-067521894797
Ciobanu, R.
fece3510-3ecf-4e71-9228-04e00a74f701
December 2015
Ma, Xiang
e00054e2-db8d-44c6-be6c-7cf807f0f6d3
Scarpa, Fabrizio
684472c3-1a28-478a-a388-5fd896986c1d
Peng, Hua-Xin
4f71af24-3d5b-4edf-ad53-53aa93dab4da
Allegri, Giuliano
8dd43a78-5f53-472f-853a-1b2fd7b129e4
Yuan, Jie
4bcf9ce8-3af4-4009-9cd0-067521894797
Ciobanu, R.
fece3510-3ecf-4e71-9228-04e00a74f701
Ma, Xiang, Scarpa, Fabrizio, Peng, Hua-Xin, Allegri, Giuliano, Yuan, Jie and Ciobanu, R.
(2015)
Design of a hybrid carbon fibre/carbon nanotube composite for enhanced lightning strike resistance.
Aerospace Science and Technology, 47, .
(doi:10.1016/j.ast.2015.10.002).
Abstract
This work presents a set of analytical design models to predict the electrical and mechanical properties of hybrid carbon nanotubes (CNT)/carbon-fibre (CF)/epoxy composites for potential use in fuselage and airframe constructions against lightning strike. The models are validated by experimental data from open literature. An optimization process is carried out to identify the microstructural configuration of the composite that provides the highest improvement in terms of electrical conductivity for the lowest structural weight in a CFRP fuselage design. The through-the-thickness conductivity of the composite laminate is considerably enhanced by a 2% volume fraction dispersion of CNTs within the matrix resin. The increase in the dielectric properties is accompanied by a moderate improvement of the composite mechanical performance. The hybrid CFRP/CNT composite configuration leads to a weight-efficient design solution for representative fuselage structures.
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Accepted/In Press date: 4 October 2015
e-pub ahead of print date: 15 November 2015
Published date: December 2015
Identifiers
Local EPrints ID: 479115
URI: http://eprints.soton.ac.uk/id/eprint/479115
ISSN: 1270-9638
PURE UUID: f464e002-ad4d-4d02-b7c7-31bff6f57576
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Date deposited: 20 Jul 2023 16:36
Last modified: 17 Mar 2024 04:20
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Contributors
Author:
Xiang Ma
Author:
Fabrizio Scarpa
Author:
Hua-Xin Peng
Author:
Giuliano Allegri
Author:
Jie Yuan
Author:
R. Ciobanu
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