Healing of a glass fibre reinforced composite with a disulphide containing organic-inorganic epoxy matrix

Journal Article (2017)
Author(s)

W. Post (TU Delft - Novel Aerospace Materials)

A. Cohades (École Polytechnique Fédérale de Lausanne)

V Michaud (École Polytechnique Fédérale de Lausanne)

Sybrand Van der ZWAAG (TU Delft - Novel Aerospace Materials)

SJ García (TU Delft - Novel Aerospace Materials)

Research Group
Novel Aerospace Materials
Copyright
© 2017 W. Post, A. Cohades, V Michaud, S. van der Zwaag, Santiago J. Garcia
DOI related publication
https://doi.org/10.1016/j.compscitech.2017.09.017
More Info
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Publication Year
2017
Language
English
Copyright
© 2017 W. Post, A. Cohades, V Michaud, S. van der Zwaag, Santiago J. Garcia
Research Group
Novel Aerospace Materials
Volume number
152
Pages (from-to)
85-93
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Abstract

We report the development of an intrinsic healing glass fibre reinforced polymer (GFRP) composite based on a disulphide-containing organic-inorganic thermoset matrix. Thermomechanical experiments showed that the newly developed matrix has a combination of a Young's modulus value in the range of (800–1200 MPa), the ability to multiple thermally induced healing delamination (70–85 °C), and processability by conventional vacuum infusion process that is not yet reported in literature. The composite mechanical properties and the extent of healing were determined by flexural, fracture and low-velocity impact testing. Small sized (<cm2) damage could be partially healed multiple times using a minimal healing pressure to ensure a good alignment of the damaged interfaces. The level of healing can be enhanced, even for large (>cm2) damage, by increasing the healing pressure provided the location of the primary damage is concentrated within the matrix phase. The polymer matrix composite introduced here represents a significant step forward from the often mechanically inferior intrinsically self-healing composites towards structural self-healing composites.

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