| タイトル | Energy Efficient Engine: Control system preliminary definition report |
| 本文（外部サイト） | http://hdl.handle.net/2060/19900019253 |
| 著者（英） | Howe, David C. |
| 著者所属（英） | Pratt and Whitney Aircraft |
| 発行日 | 1986-09-01 |
| 言語 | eng |
| 内容記述 | The object of the Control Preliminary Definition Program was to define a preliminary control system concept as a part of the Energy Efficient Engine program. The program was limited to a conceptual definition of a full authority digital electronic control system. System requirements were determined and a control system was conceptually defined to these requirements. Areas requiring technological development were identified and a plan was established for implementing the identified technological features, including a control technology demonstration. A significant element of this program was a study of the potential benefits of closed-loop active clearance control, along with laboratory tests of candidate clearance sensor elements for a closed loop system. |
| NASA分類 | AIRCRAFT PROPULSION AND POWER |
| レポートNO | 90N28569
NAS 1.26:179578
PWA-5594-331
NASA-CR-179578 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/136336 |
