| タイトル | Advantage of resonant power conversion in aerospace applications |
| 本文（外部サイト） | http://hdl.handle.net/2060/19830019723 |
| 著者（英） | Hansen, I. G. |
| 著者所属（英） | NASA Lewis Research Center |
| 発行日 | 1983-05-01 |
| 言語 | eng |
| 内容記述 | An ultrasonic, sinusoidal aerospace power distribution system is shown to have many advantages over other candidate power systems. These advantages include light weight, ease of fault clearing, versatility in handling many loads including motors, and the capability of production within the limits of present technology. References are cited that demonstrate the state of resonant converter technology and support these conclusions. |
| NASA分類 | AIRCRAFT PROPULSION AND POWER |
| レポートNO | 83N27994
NASA-TM-83399
E-1676
NAS 1.15:83399 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/162239 |
