Abstract

Three-dimensional carbon fiber reinforced silicon oxycarbide (3D Cf/SiOC) composites were fabricated through precursor infiltration and pyrolysis processing (PIP) using siloxane resin as precursor. These composites were further annealed at various temperatures to investigate their microstructure and mechanical property evolutions. It was found that the annealing temperature played a crucial role on the microstructure and mechanical properties of Cf/SiOC composites. When the annealing temperature increased from 1200 to 1400 °C, the mechanical properties of composites did not change too much, despite the matrixes underwent a redistribution of Si–O bonds and Si–C bonds. At temperature above 1500 °C, both the flexural strength and modulus decreased rapidly. This behavior was directly related to the weight loss and volume shrinkage of matrixes caused by carbothermal reductions occurred in matrixes.

Full Text
Paper version not known

Talk to us

Join us for a 30 min session where you can share your feedback and ask us any queries you have

Schedule a call

Disclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.