Processing and Mechanics of Aromatic Vitrimeric Composites at Elevated Temperatures and Healing Performance

Author:

Mandal Tanaya1ORCID,Ozten Unal2ORCID,Vaught Louis3ORCID,Meyer Jacob L.4ORCID,Amiri Ahmad56ORCID,Polycarpou Andreas35ORCID,Naraghi Mohammad2ORCID

Affiliation:

1. Department of Materials Science & Engineering, Texas A&M University, College Station, TX 77843, USA

2. Department of Aerospace Engineering, Texas A&M University, College Station, TX 77843, USA

3. J. Mike Walker ’66 Mechanical Engineering Department, Texas A&M University, College Station, TX 77843, USA

4. ATSP Innovations, Houston, TX 77055, USA

5. Russell School of Chemical Engineering, The University of Tulsa, Tulsa, OK 74104, USA

6. Department of Mechanical Engineering, The University of Tulsa, Tulsa, Oklahoma 74104, USA

Abstract

Carbon fiber reinforced polymer (CFRP) composites are renowned for their exceptional mechanical properties, with applications in industries such as automotive, aerospace, medical, civil, and beyond. Despite these merits, a significant challenge in CFRPs lies in their repairability and maintenance. This study, for the first time, delves into the processing and self-healing capability of aromatic thermosetting co-polyester vitrimer-based carbon fiber composites through mechanical testing. Vitrimers are an emerging class of thermosetting polymers, which, owing to their exchangeable covalent bonds, enable the re-formation of bonds across cracks. The specific vitrimer chosen for this study is an aromatic thermosetting co-polyester (ATSP). The mechanical properties of samples were analyzed initially through three-point bending (3PB) testing at room temperature before and after healing (by curing samples for 2 h at 280 °C). Samples were also 3PB tested at 100 °C to analyze their mechanical properties at an elevated temperature for comparison to the samples tested at room temperature. To investigate the fracture properties, optical microscopy images of samples were taken after 3PB tests, which were analyzed to observe crack initiation and crack growth behavior. Through load–displacement curves from double cantilever beam (DCB) mechanical testing, the Mode I crack initiation fracture toughness values of self-healed composites and control composites were calculated to evaluate healing efficiency in ATSP CFRP composites cured at 280 °C for 2 h. Scanning electron microscopy (SEM) showed a similar surface morphology of cracks before and after self-healing. Micro-computed tomography (CT) X-ray imaging confirmed that the healed samples closely resembled the as-fabricated ones, with the exception of some manufacturing voids, caused by outgassing in the initial healing cycle. This research demonstrated the ability for the in situ repair of ATSP CFRPs by restoring the fracture toughness to values comparable to the pristine composite (~289 J/m2).

Funder

Air Force Office of Scientific Research

Publisher

MDPI AG

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