| タイトル | Research of CMC application to turbine components |
| その他のタイトル | Research of CMC application to turbine components |
| 著者（日） | 田村 崇; 中村 武志; 高橋 耕雲; 荒木 隆人; 夏村 匡 |
| 著者（英） | Tamura, Takashi; Nakamura, Takeshi; Takahashi, Koun; Araki, Takahito; Natsumura, Tadashi |
| 著者所属（日） | 石川島播磨重工業 航空宇宙事業本部 技術開発センター; 石川島播磨重工業 航空宇宙事業本部 技術開発センター; 石川島播磨重工業 航空宇宙事業本部 技術開発センター; 石川島播磨重工業 航空宇宙事業本部 品質システム部; 石川島播磨重工業 航空宇宙事業本部 防衛システム事業部 |
| 著者所属（英） | Ishikawajima-Harima Heavy Industries Co. Ltd. Research and Engineering Division, Aero-Engine and Space Operations; Ishikawajima-Harima Heavy Industries Co. Ltd. Research and Engineering Division, Aero-Engine and Space Operations; Ishikawajima-Harima Heavy Industries Co. Ltd. Research and Engineering Division, Aero-Engine and Space Operations; Ishikawajima-Harima Heavy Industries Co. Ltd. Quality System Department, Aero-Engine and Space Operations; Ishikawajima-Harima Heavy Industries Co. Ltd. Defense Systems Division, Aero-Engine and Space Operations |
| 発行日 | 2005-08-01 |
| 刊行物名 | IHI Engineering Review
IHI Engineering Review |
| 巻 | 38 |
| 号 | 2 |
| 開始ページ | 58 |
| 終了ページ | 62 |
| 刊行年月日 | 2005-08-01 |
| 言語 | eng |
| 抄録 | Ceramics Matrix Composite (CMC) is an advanced material that has low density and high temperature capability. Application of CMC to turbine components is expected to reduce the weight and the fuel consumption of aircraft jet engine. Research and development was conducted to apply this material to the turbine shroud and vane. Coating technology was developed to protect the CMC shroud from high temperature main gas flow. These CMC shrouds were installed in an engine demonstration test at turbine inlet temperature 1,923 K. A manufacturing process for the CMC vane was developed. Burner rig test for the airfoil section was conducted to estimate the thermal cycle durability of the CMC vane. |
| キーワード | turbine component; ceramic matrix composite; CMC shroud; gas turbine; engine test; silicon carbide; thermal cycle durability; guide vane; タービン部品; セラミック基複合材料; CMCシュラウド; ガスタービン; エンジン試験; 炭化珪素; 熱サイクル耐久性; 案内羽根 |
| 資料種別 | Journal Article |
| ISSN | 0018-9820 |
| SHI-NO | AA0048286002 |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/34026 |
