Fundamental study of suspension plasma sprayed silicate coatings

Ryotaro Yanaoka, Yuji Ichikawa, Kazuhiro Ogawa, Takaya Masuda, Kazuto Sato

研究成果: Article査読

2 被引用数 (Scopus)

抄録

It is predicted that the operating temperatures of next-generation aircraft engines will exceed the present critical temperatures of any of the conventional metallic materials (<1400°C). As a result, it is likely that the application of SiC/SiC ceramic matrix composites (CMC) as primary materials. When exposed to an oxidative environment, SiC forms a protective silica scale. This layer provides additional protection from problems that may occur upon oxidation. It will, however, react with the water vapor formed during the combustion process, creating gaseous silicon hydroxides that will reduce its thickness. This problem has hindered the practical realization of CMC engines in aircrafts. Consequently, environmental barrier coatings (EBCs) are required to protect CMC components from oxidative degradation and thus ensure the reliability of CMC engines. In this study, a new deposition process, namely, the suspension plasma spray (SPS) process, is proposed to form the EBC. It produces much denser coatings by feeding a suspension of particles that are a single micron in size. It was confirmed that the coating structure and composition resulting from the SPS process were largely influenced by the residence time of the suspensions in the plasma flame. Subsequently, the optimum spray conditions were examined and discussed.

本文言語English
ページ(範囲)1390-1395
ページ数6
ジャーナルMaterials Transactions
61
7
DOI
出版ステータスPublished - 2020 7月 1

ASJC Scopus subject areas

  • 材料科学(全般)
  • 凝縮系物理学
  • 材料力学
  • 機械工学

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