High-performance ceramic thermal barrier coatings for carbon fiber-reinforced plastics developed by atmospheric plasma spraying

Authors
Praveen, KandasamyKim, HeejinLee, JuhyeongCha, Ji-HyunLee, Min Wook
Issue Date
2026-02
Publisher
Pergamon Press Ltd.
Citation
Composites Part A: Applied Science and Manufacturing, v.201
Abstract
Developing ceramic-based thermal barrier coatings (TBCs) on the fabric materials is challenging because they lack stable surfaces for achieving high-quality coatings. Herein, we propose the direct deposition of TBCs on the surface of carbon fabric, followed by the manufacturing of carbon fiber-reinforced plastic (CFRP) composite and the evaluation of its high-temperature performance. Yttrium aluminum garnet (YAG) TBCs were deposited on 3 K carbon fabric (CF) using atmospheric plasma spray (APS). The porosity of the coatings was tailored using a poreforming agent, polyether ether ketone (PEEK), and the CFRP composite was manufactured through the vacuumassisted resin transfer molding (VARTM) process. The thermal barrier performance of the resulting CFRP-TBC composite was evaluated at various temperatures, and its mechanical properties were also assessed. The porous YAG TBC, with a porosity of approximately 35 %, exhibited a reduced thermal conductivity of 0.57-0.64 W/m & sdot;K in the 25-400 degrees C range. The thermal barrier performance tests revealed that the back-surface temperature of the CFRP-TBC composite specimen ranged from 253 to 305 degrees C, while the flame temperature was approximately 500-700 degrees C. The composite maintained its initial strength up to 500 degrees C and retained about 25 % even after exposure to 700 degrees C. This study demonstrates the feasibility of integrating porous YAG TBCs directly onto CFs to enhance the high-temperature resistance of CFRP composites while maintaining manufacturability through conventional VARTM processing.
Keywords
YTTRIUM-ALUMINUM-GARNET; ADHESION STRENGTH; PVD COATINGS; BOND COAT; CONDUCTIVITY; BEHAVIOR; EROSION; TEMPERATURE; OXIDATION; POLYMERS; Plasma spray; Carbon fabric; Thermal conductivity; Mechanical properties
ISSN
1359-835X
URI
https://pubs.kist.re.kr/handle/201004/153851
DOI
10.1016/j.compositesa.2025.109424
Appears in Collections:
KIST Article > 2026
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