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Effects of high-temperature annealing on the microstructures and mechanical properties of C/C–ZrC–SiC composites prepared by precursor infiltration and pyrolysis

C/C–ZrC–SiC composites were fabricated by precursor infiltration and pyrolysis (PIP) process. A mixture solution of organic zirconium-containing polymer and polycarbosilane was chosen as the precursor. The porous carbon/carbon (C/C) preforms were first infiltrated in the precursor under vacuum, drie...

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Published in:Materials & design 2016, Vol.90, p.373-378
Main Authors: Ma, Chunhong, Guo, Lingjun, Li, Hejun, Tan, Wenlong, Duan, Tao, Liu, Ningkun, Zhang, Maoyan
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cited_by cdi_FETCH-LOGICAL-c339t-6c9a1884b6e7e1a86b993c4ee95b898a053295928bfe604040b07eca617bda653
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creator Ma, Chunhong
Guo, Lingjun
Li, Hejun
Tan, Wenlong
Duan, Tao
Liu, Ningkun
Zhang, Maoyan
description C/C–ZrC–SiC composites were fabricated by precursor infiltration and pyrolysis (PIP) process. A mixture solution of organic zirconium-containing polymer and polycarbosilane was chosen as the precursor. The porous carbon/carbon (C/C) preforms were first infiltrated in the precursor under vacuum, dried under 80°C and then pyrolyzed at 1500°C. After 20cycles of PIP process, C/C–ZrC–SiC composites were obtained. The composites were further treated at 1650°C and 1800°C at an argon atmosphere for 2h, respectively. The effects of high-temperature annealing on the microstructures and mechanical properties of C/C–ZrC–SiC composites were investigated. Results show that the density decreases and the different ceramic phases of the matrix get separated gradually as the annealing temperature increases. The mechanical strength decreases slightly after annealed at 1650°C, and the downward trend is more obvious under 1800°C in comparison to the unannealed composites. The fracture behavior of the composites changes after heat treatment. The decline of the strength and the change of the mechanical behaviors are attributed to the microstructural changes which include pores, cracks, fiber damage, weak interfacial bonding and ceramic phase separation caused by the annealing. [Display omitted] •The ceramic phases got separated gradually as annealing temperature increased.•The heat treatment decreased the mechanical properties of the C/C–ZrC–SiC composites.•The bending fracture behavior turned to non-brittle from initially brittle.
doi_str_mv 10.1016/j.matdes.2015.10.140
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source ScienceDirect Freedom Collection 2022-2024
subjects Annealing
C/C–ZrC–SiC composites
Carbon
Compressive properties
Flexural properties
Fracture mechanics
High-temperature annealing
Infiltration
Mechanical properties
Microstructure
Precursors
Pyrolysis
title Effects of high-temperature annealing on the microstructures and mechanical properties of C/C–ZrC–SiC composites prepared by precursor infiltration and pyrolysis
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