| タイトル | Advanced secondary power system for transport aircraft |
| 本文（外部サイト） | http://hdl.handle.net/2060/19850020632 |
| 著者（英） | Plencner, R. M.; Hansen, I. G.; Dengler, R. P.; Jefferies, K. S.; Hoffman, A. C.; Frye, R. J.; Beach, R. F. |
| 著者所属（英） | NASA Lewis Research Center |
| 発行日 | 1985-05-01 |
| 言語 | eng |
| 内容記述 | A concept for an advanced aircraft power system was identified that uses 20-kHz, 440-V, sin-wave power distribution. This system was integrated with an electrically powered flight control system and with other aircraft systems requiring secondary power. The resulting all-electric secondary power configuration reduced the empty weight of a modern 200-passenger, twin-engine transport by 10 percent and the mission fuel by 9 percent. |
| NASA分類 | AIRCRAFT PROPULSION AND POWER |
| レポートNO | 85N28944
E-2434
NASA-TP-2463
NAS 1.60:2463 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/156186 |
