The invention provides a power supply system of an aircraft and a control method of the power supply system of the aircraft. The power supply system of the aircraft comprises a fuel cell configured to generate electric energy; a converter device configured to supply the 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 according to a predetermined driving mode; a battery configured to supply a voltage to a second motor device for driving the aircraft through a second output terminal, the second output terminal being connected to the output node of the fuel cell; and a processor configured to control a connection between the fuel cell and the converter device according to the driving mode.
本公开提供了一种飞行器的供电系统和飞行器的供电系统的控制方法。该飞行器的供电系统包括:燃料电池,被配置为产生电能;转换器装置,被配置为通过第一输出端子将燃料电池产生的电压供应至用于驱动飞行器的第一电机装置,并根据预定的驱动模式切换与燃料电池的连接;电池,被配置为通过第二输出端子将电压供应至用于驱动飞行器的第二电机装置,第二输出端子与燃料电池的输出节点连接;以及处理器,被配置为根据驱动模式控制燃料电池和转换器装置之间的连接。
Power supply system of aircraft and control method of power supply system of aircraft
飞行器的供电系统和飞行器的供电系统的控制方法
2024-05-14
Patent
Elektronische Ressource
Chinesisch
IPC: | H02J CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER , Schaltungsanordnungen oder Systeme für die Abgabe oder Verteilung elektrischer Leistung / B60L PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES , Antrieb von elektrisch angetriebenen Fahrzeugen / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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