A power supply system for an aircraft and a control method thereof are provided. The power supply system of the aircraft includes a fuel cell configured to generate electrical energy, a converter device configured to supply a voltage generated by the fuel cell to a first motor device for driving the aircraft through a first output terminal and switch a connection with the fuel cell depending on a predetermined driving mode, a battery configured to supply the voltage to a second motor device for driving the aircraft through a second output terminal, the second output terminal being connected with an output node of the fuel cell, and a processor configure to control a connection between the fuel cell and the converter device depending on the driving mode.
POWER SUPPLY SYSTEM OF AIRCRAFT AND CONTROL METHOD THEREOF
STROMVERSORGUNGSSYSTEM FÜR EIN FLUGZEUG UND STEUERVERFAHREN DAFÜR
SYSTÈME D'ALIMENTATION ÉLECTRIQUE D'AÉRONEF ET SON PROCÉDÉ DE COMMANDE
2024-06-12
Patent
Electronic Resource
English
Power Supply System of Aircraft and Control Method Thereof
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