An aircraft power control device for controlling electric power in an aircraft includes a DC/DC-converter configured for receiving a DC input voltage on a converter input side, converting the received DC input voltage into a DC output voltage and outputting the DC output voltage on a converter output side and an electric power switch is electrically coupled to the converter output side of the DC/DC-converter. The electric power switch is switchable between a switched-on state and a switched-off state. The switch output side is electrically coupled with the switch input side of the electric power switch when in the switched-on state, and wherein the switch output side is electrically isolated from the switch input side of the electric power switch, when in the switched-off state. The system also includes a monitoring device to control the state of the switch.
AIRCRAFT POWER CONTROL DEVICE, AIRCRAFT COMPRISING AN AIRCRAFT POWER CONTROL DEVICE, AND METHOD OF CONTROLLING AN AIRCRAFT POWER CONTROL DEVICE
2025-03-06
Patent
Electronic Resource
English
IPC: | H02M APPARATUS FOR CONVERSION BETWEEN AC AND AC, BETWEEN AC AND DC, OR BETWEEN DC AND DC, AND FOR USE WITH MAINS OR SIMILAR POWER SUPPLY SYSTEMS , Anlagen zur Umformung von Wechselstrom in Wechselstrom, von Wechselstrom in Gleichstrom oder umgekehrt, oder von Gleichstrom in Gleichstrom und zur Verwendung in Netzen oder ähnlichen Stromversorgungssystemen / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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