To provide a fuel cell equipped drone that can use the electric power of a fuel cell and a secondary battery according to required electric power.SOLUTION: A fuel cell equipped drone 11 has: a flight electric motor 24; a hydrogen fuel cell 42 that generates electric power to be supplied to the flight electric motor 24; and a secondary battery 46 that supplies electric power to the flight electric motor 24. The fuel cell equipped drone 11 is configured to have: a switching unit 44 that can switch between a low load mode in which electric power from the hydrogen fuel cell 42 is supplied to the flight electric motor 24 and a high load mode in which electric power from the hydrogen fuel cell 42 and electric power from the secondary battery 46 are supplied to the flight electric motor 24; and a control unit 45 that determines whether or not the electric power required by the flight electric motor 24 is equal to or less than the power generated by the hydrogen fuel cell 42, wherein the control unit 45 also selects the low load mode if the required electric power is equal to or less than the generated electric power, or selects the high load mode if the required electric power exceeds the generated electric power.SELECTED DRAWING: Figure 1

    【課題】必要電力に応じて燃料電池及び二次電池の電力を利用することが可能な燃料電池搭載ドローンを提供する。【解決手段】飛行用電動モータ24と、飛行用電動モータ24に供給する電力を発生する水素燃料電池42と、電力を飛行用電動モータ24へ供給する二次電池46と、を有する燃料電池搭載ドローン11であって、水素燃料電池42の電力を飛行用電動モータ24へ供給する低負荷モードと、水素燃料電池42の電力及び二次電池46の電力を飛行用電動モータ24へ供給する高負荷モードと、を切り替えできる切替部44と、飛行用電動モータ24の必要電力が水素燃料電池42の発生電力以下であるか否かを判断する制御部45と、必要電力が発生電力以下であると低負荷モードを選択し、必要電力が発生電力を超えると高負荷モードを選択する制御部45と、を有する燃料電池搭載ドローン11を構成した。【選択図】図1


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    Titel :

    FUEL CELL EQUIPPED DRONE


    Weitere Titelangaben:

    燃料電池搭載ドローン


    Beteiligte:
    SASAKI HIROYUKI (Autor:in) / HORII TATSUKI (Autor:in) / MIYAMOTO TSUBASA (Autor:in)

    Erscheinungsdatum :

    28.11.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Japanisch


    Klassifikation :

    IPC:    B64U / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / H02J CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER , Schaltungsanordnungen oder Systeme für die Abgabe oder Verteilung elektrischer Leistung



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