Two-matrix composites: Carbon fiber micropultrusions embedded in flexible epoxy matrices

Two-matrix composites: Carbon fiber micropultrusions embedded in flexible epoxy matrices

Callens, S.J.P. (TU Delft Biomaterials & Tissue Biomechanics; TU Delft Aerospace Engineering)
Bergsma, O.K. (TU Delft Structural Integrity & Composites)

Aerospace Engineering

2018

Two-matrix composites combine fibers with two distinct matrices. This is achieved by impregnating fiber bundles with a high-stiffness matrix and embedding the cured bundles in a flexible matrix. Two-matrix composites have been shown to offer unprecedented combinations of transverse flexibility and longitudinal tensile strength, and could offer improved fiber alignment and manufacturability. Here, we explore this concept further by embedding carbon fiber micropultrusions in flexibilized epoxy matrices and examining the longitudinal compression behavior. Our results on thin-walled rings reveal that the failure mode depends on micropultrusion diameter, with small diameters resulting in micropultrusion kinking and larger diameters in splitting and crushing. Additionally, we find that two-matrix composites can offer higher compression strength than conventional composites with the same flexible matrix, despite a lower fiber volume fraction. The inherent manufacturing advantages and high anisotropy could make two-matrix composites interesting candidates for specific applications, such as morphing wings or additively manufactured composites.

Mechanical testing (D)
Filament winding (E)
Mechanical properties (B)
Transverse cracking (B)

http://resolver.tudelft.nl/uuid:b1a85c4f-cfc9-4253-9bcc-e3f1940dbc5d

https://doi.org/10.1016/j.compositesa.2018.08.008

2020-08-10

1359-835X

Composites Part A: Applied Science and Manufacturing, 114, 1-12

Institutional Repository

journal article

© 2018 S.J.P. Callens, O.K. Bergsma