Full metadata record
| DC Field | Value | Language |
|---|---|---|
| dc.contributor.author | Praveen, Kandasamy | - |
| dc.contributor.author | Kim, Heejin | - |
| dc.contributor.author | Lee, Juhyeong | - |
| dc.contributor.author | Cha, Ji-Hyun | - |
| dc.contributor.author | Lee, Min Wook | - |
| dc.date.accessioned | 2025-12-23T06:30:05Z | - |
| dc.date.available | 2025-12-23T06:30:05Z | - |
| dc.date.created | 2025-12-19 | - |
| dc.date.issued | 2026-02 | - |
| dc.identifier.issn | 1359-835X | - |
| dc.identifier.uri | https://pubs.kist.re.kr/handle/201004/153851 | - |
| dc.description.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. | - |
| dc.language | English | - |
| dc.publisher | Pergamon Press Ltd. | - |
| dc.title | High-performance ceramic thermal barrier coatings for carbon fiber-reinforced plastics developed by atmospheric plasma spraying | - |
| dc.type | Article | - |
| dc.identifier.doi | 10.1016/j.compositesa.2025.109424 | - |
| dc.description.journalClass | 3 | - |
| dc.identifier.bibliographicCitation | Composites Part A: Applied Science and Manufacturing, v.201 | - |
| dc.citation.title | Composites Part A: Applied Science and Manufacturing | - |
| dc.citation.volume | 201 | - |
| dc.description.isOpenAccess | Y | - |
| dc.identifier.wosid | 001621888100002 | - |
| dc.identifier.scopusid | 2-s2.0-105021939050 | - |
| dc.relation.journalWebOfScienceCategory | Engineering, Manufacturing | - |
| dc.relation.journalWebOfScienceCategory | Materials Science, Composites | - |
| dc.relation.journalResearchArea | Engineering | - |
| dc.relation.journalResearchArea | Materials Science | - |
| dc.type.docType | Article | - |
| dc.subject.keywordPlus | YTTRIUM-ALUMINUM-GARNET | - |
| dc.subject.keywordPlus | ADHESION STRENGTH | - |
| dc.subject.keywordPlus | PVD COATINGS | - |
| dc.subject.keywordPlus | BOND COAT | - |
| dc.subject.keywordPlus | CONDUCTIVITY | - |
| dc.subject.keywordPlus | BEHAVIOR | - |
| dc.subject.keywordPlus | EROSION | - |
| dc.subject.keywordPlus | TEMPERATURE | - |
| dc.subject.keywordPlus | OXIDATION | - |
| dc.subject.keywordPlus | POLYMERS | - |
| dc.subject.keywordAuthor | Plasma spray | - |
| dc.subject.keywordAuthor | Carbon fabric | - |
| dc.subject.keywordAuthor | Thermal conductivity | - |
| dc.subject.keywordAuthor | Mechanical properties | - |
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