Ablation behavior of functional gradient ceramic coating for porous carbon-bonded carbon fiber composites
Creators
- 1. Science and Technology on High Strength Structure Materials Laboratory, Central South University, Changsha 410083 (China)
- 2. Science and Technology of Advanced Functional Composite Laboratory, Aerospace Research Institute of Materials & Technology, Beijing 100076 (China)
Description
Highlights: • A novel functional gradient ceramic coating was prepared to improve the ablation resistance of CBCF composites at high temperature. This coating consists a two layer structure with a compact HfB2-MoSi2 outer layer (150∼200 μm in thick) and an inner Si-CBCF layer (2∼3 mm in thick). The ablation resistance of the coated CBCF composites was investigated with an arc-jet testing at temperature 1500-2200 °C. No macro-cracks and carbon fibers are detected in the cyclic ablation regions. The mass of sample was slightly reduced and the mass ablative rate was only 5.8′10−4g/(cm2∙s). Meanwhile, the thickness of the sample didn't change obviously, indicating good ablation resistance and good thermal shock resistance of the functional gradient ceramic coated CBCF composite. After ablation, the surface coating exhibit three different ablation regions due to the different ablation temperature. The formation of a dense silica glass layer embedded with HfO2 particles or a molten HfO2 layer was responsible for the good ablation resistant to the functional gradient ceramic coating. - Abstract: To improve the ablation resistance of low density carbon bonded carbon fiber (CBCF) composites at high temperature, a novel functional gradient ceramic coating was prepared. The coating exhibits a two layer structure with a compact HfB2-MoSi2 outer layer and an inner Si-CBCF layer with gradient transition structure. The high temperature ablation resistance of the coated CBCF composites was investigated with an arc-jet testing at temperature 1500–2200 °C. The results showed that the prepared functional ceramic coating exhibited good ablation resistance and good thermal shock resistance after four ablation cycles. After ablation, the surface coating exhibit three different ablation regions due to the different ablation temperature. The formation of a dense silica glass layer embedded with HfO2 particles or a molten HfO2 layer was responsible for the good ablation resistant to the functional gradient ceramic coating.
Availability note (English)
Available from http://dx.doi.org/10.1016/j.corsci.2018.07.025Additional details
Identifiers
- DOI
- 10.1016/j.corsci.2018.07.025;
- PII
- S0010938X17322059;
Publishing Information
- Journal Title
- Corrosion Science
- Journal Volume
- 142
- Journal Page Range
- p. 145-152
- ISSN
- 0010-938X
- CODEN
- CRRSAA
INIS
- Country of Publication
- United Kingdom
- Country of Input or Organization
- International Atomic Energy Agency (IAEA)
- INIS RN
- 50048876
- Subject category
- S36: MATERIALS SCIENCE;
- Descriptors DEI
- CARBON; CARBON FIBERS; CERAMICS; COATINGS; COMPOSITE MATERIALS; GLASS; HAFNIUM BORIDES; HAFNIUM OXIDES; LAYERS; MOLYBDENUM SILICIDES; POROUS MATERIALS; SURFACE COATING; SURFACES; THERMAL SHOCK; THICKNESS
- Descriptors DEC
- BORIDES; BORON COMPOUNDS; CHALCOGENIDES; DEPOSITION; DIMENSIONS; ELEMENTS; FIBERS; HAFNIUM COMPOUNDS; MATERIALS; MOLYBDENUM COMPOUNDS; NONMETALS; OXIDES; OXYGEN COMPOUNDS; REFRACTORY METAL COMPOUNDS; SILICIDES; SILICON COMPOUNDS; TRANSITION ELEMENT COMPOUNDS
Optional Information
- Copyright
- Copyright (c) 2017 Elsevier Science B.V., Amsterdam, The Netherlands, All rights reserved.