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.
Advanced Secondary Power System for Transport Aircraft
1985
38 pages
Report
Keine Angabe
Englisch
Advanced secondary power system for transport aircraft
NTRS | 1985
|Secondary Power Generation System Considerations for Advanced Aircraft
SAE Technical Papers | 1984
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