The hydrogen power fuel cell structure for the unmanned aerial vehicle comprises a cell shell, an electric pile and an air driving part, an air passing groove is formed in the cell shell, and the electric pile is matched with the air passing groove, so that all air flowing into the cell shell flows into the electric pile through the air passing groove, and the reaction efficiency of the electric pile is improved; the air driving part is mounted on the battery shell, air generated after the galvanic pile is driven to react is discharged out of the battery shell through the air driving part, and after the reacted air is discharged, the air pressure in the battery shell is reduced, and external air flows into the battery shell under the action of atmospheric pressure.

    一种用于无人机的氢动力燃料电池结构,所述氢动力燃料电池结构包括电池壳体、电堆和空气驱动件,电池壳体内成形有过气槽,电堆与过气槽适配,使得流入电池壳体内的所有空气都通过过气槽流入电堆内,提高电堆的反应效率;空气驱动件安装在电池壳体上,通过空气驱动件将驱动电堆反应后的空气排出电池壳体外,反应后的空气排出后,电池壳体内气压下降,外部空气受到大气压力的作用流入电池壳体内。


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    Titel :

    Hydrogen power fuel cell structure for unmanned aerial vehicle


    Weitere Titelangaben:

    一种用于无人机的氢动力燃料电池结构


    Beteiligte:
    XU WEIQIANG (Autor:in) / GAO DING (Autor:in) / GONG KUNYING (Autor:in)

    Erscheinungsdatum :

    02.12.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / 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



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