The invention provides a fuel cell system and an aircraft capable of charging a storage battery while ensuring independence and redundancy of the fuel cell and the storage battery as power sources. The fuel cell system is a fuel cell system for an aircraft, and is characterized in that the fuel cell system comprises a fuel cell, a storage battery, a motor, and a control unit, the motor connects the fuel cell and the storage battery through a circuit as an independent power source, and the motor has a dual three-phase winding using dual inverters. When a normal output request from the motor is received, the control unit drives the motor with a predetermined first output from the fuel cell, and charges the battery with a torque generated by the motor.

    本发明提供能够在保证燃料电池与蓄电池的作为电源的独立性和冗余性的同时进行对蓄电池的充电的燃料电池系统和飞行器。该燃料电池系统是飞行器用的燃料电池系统,其特征在于,上述燃料电池系统具有燃料电池、蓄电池、马达以及控制部,上述马达通过电路连接上述燃料电池与上述蓄电池作为独立的电源,并且具有使用了双逆变器的双重3相绕组,上述控制部在收到来自上述马达的通常输出要求时以来自上述燃料电池的规定的第1输出驱动上述马达,并且借助由上述马达产生的扭矩对上述蓄电池进行充电。


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    Titel :

    Fuel cell system and aircraft


    Weitere Titelangaben:

    燃料电池系统和飞行器


    Beteiligte:
    OKABE HIROKI (Autor:in) / SAITO KIMIO (Autor:in)

    Erscheinungsdatum :

    25.10.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    H01M Verfahren oder Mittel, z.B. Batterien, für die direkte Umwandlung von chemischer in elektrische Energie , PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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