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Cyclic-Dependent Damage Evolution in Self-Healing Woven SiC/[Si-B-C] Ceramic-Matrix Composites at Elevated Temperatures

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College of Civil Aviation, Nanjing University of Aeronautics and Astronautics, No.29, Yudao St., Nanjing 210016, China
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Université de Lyon, INSA-Lyon, MATEIS (UMR CNRS 5510), 7 Avenue Jean Capelle, 69621 Villeurbanne Cedex, France
*
Author to whom correspondence should be addressed.
Materials 2020, 13(6), 1478; https://doi.org/10.3390/ma13061478
Received: 29 January 2020 / Revised: 10 March 2020 / Accepted: 18 March 2020 / Published: 24 March 2020
Cycle-dependent damage evolution in self-healing, 2.5D woven Hi-NicalonTM SiC/[Si-B-C] and 2D woven Hi-NicalonTM SiC/[SiC-B4C] ceramic-matrix composites (CMCs) at 600 and 1200 °C was investigated. The cycle-dependent damage parameters of internal friction, dissipated energy, Kachanov’s damage parameter, and broken fiber fraction were obtained to describe damage development in self-healing CMCs. The relationships between cycle-dependent damage parameters and multiple fatigue damage mechanisms were established. The experimental fatigue damage development of self-healing Hi-NicalonTM SiC/[Si-B-C] and Hi-NicalonTM SiC/[SiC-B4C] composites was predicted for different temperatures, peak stresses, and loading frequencies. The cycle-dependent damage evolution of self-healing Hi-NicalonTM SiC/[Si-B-C] and Hi-NicalonTM SiC/[SiC-B4C] composites depends on temperature, testing environment, peak stress, and loading frequency. For the Hi-NicalonTM SiC/[Si-B-C] composite, temperature is a governing parameter for the fatigue process. At an elevated temperature of 600 °C in an air atmosphere, the internal frictional parameter of Hi-NicalonTM SiC/[Si-B-C] composite decreases first and then increases with applied cycle number; however, at an elevated temperature of 1200 °C in an air atmosphere, the internal frictional parameter of Hi-NicalonTM SiC/[Si-B-C] composite decreases with applied cycle number, and the interface shear stress at 1200 °C is much lower than that at 600 °C. For Hi-NicalonTM SiC/[SiC-B4C] composite at 1200 °C, loading frequency is a governing parameter for the fatigue process. The degradation rate of interface shear stress is much higher at the loading frequency of 0.1 Hz than that at the loading frequency of 1 Hz. View Full-Text
Keywords: ceramic-matrix composites (CMCs); Self-healing; cycle-dependent; damage evolution; damage parameters; internal friction; interface damage; fiber failure ceramic-matrix composites (CMCs); Self-healing; cycle-dependent; damage evolution; damage parameters; internal friction; interface damage; fiber failure
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MDPI and ACS Style

Li, L.; Reynaud, P.; Fantozzi, G. Cyclic-Dependent Damage Evolution in Self-Healing Woven SiC/[Si-B-C] Ceramic-Matrix Composites at Elevated Temperatures. Materials 2020, 13, 1478. https://doi.org/10.3390/ma13061478

AMA Style

Li L, Reynaud P, Fantozzi G. Cyclic-Dependent Damage Evolution in Self-Healing Woven SiC/[Si-B-C] Ceramic-Matrix Composites at Elevated Temperatures. Materials. 2020; 13(6):1478. https://doi.org/10.3390/ma13061478

Chicago/Turabian Style

Li, Longbiao, Pascal Reynaud, and Gilbert Fantozzi. 2020. "Cyclic-Dependent Damage Evolution in Self-Healing Woven SiC/[Si-B-C] Ceramic-Matrix Composites at Elevated Temperatures" Materials 13, no. 6: 1478. https://doi.org/10.3390/ma13061478

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