In a power supply system of an aircraft, when electric power is supplied from a power generation unit to a drive unit, the electric power is supplied from the power generation unit to the drive unit via a first power transmission path, and a voltage is applied to a second power transmission path by a fault detection circuit in a state in which the power generation unit and the drive unit are disconnected from the second power transmission path, and when the power generation unit is started, electric power of the fault detection circuit is supplied to the power generation unit in a state in which the power generation unit is connected to the second power transmission path.
Power supply system of aircraft
2024-08-06
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
Electric power supply system for an aircraft, aircraft and airport power supply system
European Patent Office | 2016
|Aircraft electric power-supply system
Engineering Index Backfile | 1943
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