A charging control system (70) includes a power unit having a power generation apparatus (40a) configured to perform power generation to supply electric power to a load, and a battery (32) configured to accumulate the electric power supplied from the power generation apparatus and supply the electric power that is accumulated to the load, and a control section (91) configured to apply a target power feed amount indicating an amount of power to be supplied to the load and a target power charge amount indicating an amount of power to be stored in the battery to a charge loss characteristic of the battery and a fuel consumption characteristic of the power generation apparatus to decide a fuel consumption of the power generation apparatus and to control charge of the battery based on the fuel consumption. In accordance with this, the fuel consumption can be suppressed.


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    Titel :

    CHARGING CONTROL SYSTEM, CHARGING CONTROL METHOD AND AIRCRAFT


    Beteiligte:
    TSUTSUMI DAIKO (Autor:in)

    Erscheinungsdatum :

    05.10.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B60W CONJOINT CONTROL OF VEHICLE SUB-UNITS OF DIFFERENT TYPE OR DIFFERENT FUNCTION , Gemeinsame Steuerung oder Regelung von Fahrzeug-Unteraggregaten verschiedenen Typs oder verschiedener Funktion / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B60L PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES , Antrieb von elektrisch angetriebenen Fahrzeugen



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