Internal damage evolution of C/SiC composites in air at 1650 °C studied by in-situ synchrotron X-ray imaging

Carbon fibre reinforced silicon carbide (C/SiC) ceramic matrix composites have attracted considerable attention due to their exceptional properties and extensive potential applications as high-temperature structural materials. However, due to their complex structure and manufacturing defects, C/SiC...

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Veröffentlicht in:Composites. Part B, Engineering Engineering, 2025-01, Vol.288, p.111878, Article 111878
Hauptverfasser: Xi, Li, Li, Shaoling, Xue, Kaiyuan, Cui, Xiaochuan, Wang, Bowen, Li, Ying, Fang, Daining
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Sprache:eng
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Zusammenfassung:Carbon fibre reinforced silicon carbide (C/SiC) ceramic matrix composites have attracted considerable attention due to their exceptional properties and extensive potential applications as high-temperature structural materials. However, due to their complex structure and manufacturing defects, C/SiC composites exhibit intricate mechanical behaviour under thermal-mechanical-oxidative coupling environments. To date, systematic studies on the internal damage evolution and failure mechanisms of C/SiC composites under high-temperature oxidative environments are lacking. In this study, a combination of synchrotron X-ray micro-computed tomography (SR-μCT) and in-situ experiments under thermal-mechanical-oxidative coupling environments at room temperature and 1650 °C in air was used to characterize the internal microstructures and damage evolution processes of C/SiC composites at different loading levels. Additionally, the 3D strain fields during in-situ loading were quantitatively analysed using the Digital Volume Correlation (DVC) method. The findings underscore the substantial impact of oxidative damage on the mechanical response of C/SiC composites, particularly concerning tensile properties and fracture modes. At room temperature, severe delamination, fibre bundle pull-out and interfacial debonding occurred internally. Whereas, under high-temperature atmospheric conditions, severe fibre oxidation reactions occurred at the specimen edges, resulting in rapid porosity escalation. Crack initiation from surface defects followed by rapid inward propagation is observed. Moreover, while the strain distribution remains relatively uniform until fracture, a pronounced concentration of strain is evident near the fracture zones at room temperature, with an even greater concentration observed at 1650 °C. Notably, the region of concentrated strain within the 3D deformation field corresponds closely to the final fracture location, as revealed by quantitative DVC analysis. •Novel insights into mechanical behaviour and damage evolution of PIP-C/SiC composites.•Comprehensive characterization using SR-μCT and in-situ loading reveals temperature-dependent fracture characteristics.•Distinct porosity evolution and strain distribution patterns observed at different temperatures.•Oxidative degradation modifies toughening mechanisms, impacting fracture modes.•Enhanced understanding of C/SiC composites for high-temperature applications.
ISSN:1359-8368
DOI:10.1016/j.compositesb.2024.111878