| タイトル | Gas turbine engine with convertible accessories |
| 本文（外部サイト） | http://hdl.handle.net/2060/19780009113 |
| 著者（英） | Adamson, A. P.; Sargisson, D. F. |
| 著者所属（英） | NASA Lewis Research Center|General Electric Co. |
| 発行日 | 1978-01-17 |
| 言語 | eng |
| 内容記述 | Drive means for connecting a gas turbine engine to its accessories are so constructed as to allow the accessories to be selectively positioned to any one of several predetermined circumferential positions about the perimeter of the engine. This feature permits convenient mounting of the same engine upon vehicles demanding radically different engine mounting arrangements. |
| NASA分類 | AIRCRAFT PROPULSION AND POWER |
| レポートNO | 78N17056 |
| 権利 | No Copyright |
