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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
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.
1270-9638
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
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, 367-377. (doi:10.1016/j.ast.2015.10.002).

Record type: Article

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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More information

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
ORCID for Jie Yuan: ORCID iD orcid.org/0000-0002-2411-8789

Catalogue record

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 ORCID iD
Author: R. Ciobanu

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