The invention provides a fuel cell system and an aircraft. The fuel cell system can improve the performance of a fuel cell even when the fuel cell system is high. This fuel cell system is used in an aircraft, and is characterized by being provided with: a fuel cell; an oxidant gas system for supplying an oxidant gas to the fuel cell; a height sensor; and a control unit, the oxidant gas system having an air compressor and a bypass flow path that bypasses the fuel cell, the bypass flow path having a bypass valve, and the control unit increasing the rotational speed of the air compressor and increasing the opening degree of the bypass valve when an increase in the height measured by the height sensor is detected.

    本发明提供燃料电池系统以及飞行器,该燃料电池系统在高度高的情况下也能够使燃料电池的性能提高。该燃料电池系统被用于飞行器,上述燃料电池系统的特征在于,具有:燃料电池;氧化剂气体系统,向上述燃料电池供给氧化剂气体;高度传感器;以及控制部,上述氧化剂气体系统具有空气压缩机、绕过上述燃料电池的旁通流路,上述旁通流路具有旁通阀,在检测到上述高度传感器测量出的高度的上升时,上述控制部增大上述空气压缩机的转速且增大上述旁通阀的开度。


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    Titel :

    Fuel cell system and aircraft


    Weitere Titelangaben:

    燃料电池系统以及飞行器


    Beteiligte:

    Erscheinungsdatum :

    11.11.2022


    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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