| タイトル | Laminated turbine vane design and fabrication |
| 本文（外部サイト） | http://hdl.handle.net/2060/19790025033 |
| 著者（英） | Hess, W. G. |
| 著者所属（英） | Pratt and Whitney Aircraft Group |
| 発行日 | 1979-10-19 |
| 言語 | eng |
| 内容記述 | A turbine vane and associated endwalls designed for advanced gas turbine engine conditions are described. The vane design combines the methods of convection cooling and selective areas of full coverage film cooling. The film cooling technique is utilized on the leading edge, pressure side, and endwall regions. The turbine vane involves the fabrication of airfoils from a stack of laminates with cooling passages photoetched on the surface. Cold flow calibration tests, a thermal analysis, and a stress analysis were performed on the turbine vanes. |
| NASA分類 | AIRCRAFT PROPULSION AND POWER |
| レポートNO | 79N33204
FR-11662
NASA-CR-159655 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/174493 |
