An indication system for a hybrid aircraft power plant including an electric motor and a heat engine for driving an air mover configured to propel an aircraft is provided. The indication system includes a display providing a display area and a computer operatively connected to the display. The computer is configured to cause a first visual indication to be generated in the display area of the display. The first visual indication indicates a current amount of energy stored in a battery powering the electric motor of the hybrid aircraft power plant along a scale. The computer is configured to cause a second visual indication to be generated in the same display area of the display. The second visual indication indicates a remaining run time for the electric motor based on the current amount of energy stored in the battery.


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    Titel :

    INDICATOR FOR HYBRID AIRCRAFT POWER PLANT


    Beteiligte:
    SYED YUSUF (Autor:in) / GARIEPY RAPHAEL (Autor:in) / RICCI THOMAS TREVOR (Autor:in) / YOUNG TODD (Autor:in) / TWARECKI PIOTR (Autor:in)

    Erscheinungsdatum :

    26.06.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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