A method and apparatus for operating a power architecture for an aircraft, includes a primary variable frequency generator system having a first power output, a secondary variable frequency generator system having a second power output, a power distribution node, an essential power bus selectively connected with a set of essential aircraft electrical loads, and a controller module.
METHOD AND APPARATUS FOR OPERATING A POWER SYSTEM ARCHITECTURE
2018-11-29
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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