Microstructure and oxidation behavior of sol–gel mullite coating on SiC-coated carbon/carbon composites

Zhou, Wen; Xiao, Peng; Li, Zhuan; Wen, Hu; Luo, Hang; Yu, Xiaoyu; Yang, Li; Chen, Wenbo

doi:10.1016/j.jeurceramsoc.2015.06.033

Cited by 69 publications

(2 citation statements)

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“…Therefore, carbon fiber reinforced (C/C) carbon arrays are used in materials in the aerospace industry due to their desirable characteristics such as high ablation and mechanical resistance, heat resistance, dimensional stability, high solvent resistance, acids and water, flame resistance, low smoke emission when material is incinerated, excellent ablative properties and low cost. They absorb energy as they degrade and serve as a binder for the other components (Miranda et al, 2017;Zhongliu et al, 2015;Machado, 2012). However, under re-entry conditions at high temperature oxidizing atmospheres, carbon fiber composites undergo intense thermal degradation due to the high catalytic reactions between carbon and oxygen, and in some situations make their use in aerospace devices difficult.…”

Section: Introductionmentioning

confidence: 99%

“…The formation of this oxide acts as a TPS barrier when subjected to aerothermodynamic effects to protect the C / C composite against oxidation, mass loss and consequently preserving its mechanical properties. There are several techniques used to deposit and / or coat a material according to its application, namely chemical vapor deposition, package cementation, hydrothermal electrophoretic deposition, mud methods and plasma spraying (Miranda et al, 2017;Zhongliu et al, 2015;Aparicio et al, 2000).…”

Section: Introductionmentioning

confidence: 99%

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Analysis of mullite ablative properties simulated in hypersonic plasma wind tunnel / Análise das propriedades ablativas da mulita simuladas em túnel de vento plasma hipersónico

Rita¹,

Miranda²,

Prado³

et al. 2021

BJDV

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Mullite is a ceramic composed of silicon oxide and aluminum used in various technological applications due to its physical and chemical properties, such as: Low thermal expansion, high thermal stability, low density, low thermal conductivity, good mechanical resistance and creep resistance, good stability in severe chemical environments, among other properties [1]. The supersonic plasma wind tunnel was optimized to investigate the ablative properties of the ceramic composite -Mullite (3 2 3 . 2 2 ) deposited by the plasma spray process on Carbon -Carbon Substrate (C/C). The tests were performed at low pressure in a reactive air plasma using a DC nontransferred arc plasma torch with enthalpies of 7.2MJ / kg at 18.5MJ / kg and heat fluxes of 0.52 MW/m2 to 2.2 MW/m2 (Fig. 1). The specific mass loss rate of the coated Mullite on the (C/C) was evaluated as a function of the exposure time and the heat flow. Microstructural and chemical analysis of the (C/C) substrate of the coated mullite before and after the ablation process through SEM / EDS were also performed. The mullite used in this experiment was processed by the Sol-gel method developed in the materials processing laboratory (PLASMAT-ITA), that is, a process involving a solution that passes through a transition called sol-gel and becomes gel by the and the basic objective of this technique is the preparation of a homogeneous precursor solution from which a semi -rigid gel with level of atomic homogeneity [1]. The synthesis of the mullite is obtained from the mixture in sol-gel of materials that present in its composition ( 2 3 ). From the synthesis of the Mullite Sol-gel, it was inserted in a Plasma Spray process developed in the Thermal Plasma Laboratory (PLASMAT-ITA), where it was processed the coating of the Mullite in Carbon/Carbon substrate creating a layer of thermal protection on the substrate. The analysis of the obtained results showed that the adhesion of the mullite is directly related to the exposure time of the substrate (C/C) in the plasma spray process, in the formation of the coating as a protective layer, since the analysis of the rate of mass loss and showed that the mullite deposited on the surface of the (C/C) did not show good efficiency when this protective coating was submitted to the ablation process inside the supersonic plasma wind tunnel.

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Section: Introductionmentioning

confidence: 99%

Section: Introductionmentioning

confidence: 99%