Development and characterization of a natural lightweight composite solution for aircraft structural applications

Sandwich-based structures play a major role in several transport applications due to their high stiffness and strength-to-weight ratios. Some properties of cork agglomerates suggest that this natural material may represent an excellent candidate when implemented as the core of sandwich components su...

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Bibliographic Details
Published in:Composite structures 2016-02, Vol.136, p.430-440
Main Authors: Potes, F.C., Silva, J.M., Gamboa, P.V.
Format: Article
Language:English
Subjects:
Agglomerates
Aircraft
Aircraft components
Cellular morphology
Computer simulation
Cork agglomerate
Lightweight
Loss factor
Mathematical models
Stiffness
Strain energy
Topology optimization
Weight reduction
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Summary:Sandwich-based structures play a major role in several transport applications due to their high stiffness and strength-to-weight ratios. Some properties of cork agglomerates suggest that this natural material may represent an excellent candidate when implemented as the core of sandwich components such as the ones typically adopted in aircraft interiors. However, one major drawback still resides in their higher density values in comparison to other lightweight benchmark materials. In order to address this issue, a perforated structural concept is herein presented for the cork agglomerate core as part of a weight minimization strategy. The aim of this investigation consists in assessing the influence of several core design variables, including the cells’ geometry, perforation ratio and pattern, with regard to the impact on the components’ overall mechanical stiffness and damping performance. The design process was supported by numerical simulations carried out with the ABAQUS® FEM tool and validated via experimental testing characterization. Results showed that distinct optimized cellular topologies can be derived with improved properties tailored for the functional requirements of specific components, thus confirming the validity of such cork-based composites in aircraft structural applications.
ISSN:0263-8223
1879-1085
DOI:10.1016/j.compstruct.2015.10.034