An electric vertical takeoff and landing aircraft with a plurality of electric drive systems each including a drive motor for turning a rotor and a drive unit for driving the drive motor includes: a drive information detection unit that detects, for each of the plurality of electric drive systems, drive information including at least one of motor information serving as an indicator of the deterioration state of the drive motor and drive unit information serving as an indicator of the deterioration state of the drive unit; and a maintenance necessity detection unit that detects the necessity or lack of necessity of maintenance on each of the plurality of electric drive systems based on the detected drive information.


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    Title :

    Electric vertical takeoff and landing aircraft and control device for electric vertical takeoff and landing aircraft


    Contributors:

    Publication date :

    2025-04-15


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    G07C TIME OR ATTENDANCE REGISTERS , Zeit- oder Anwesenheitskontrollgeräte / B64C AEROPLANES , Flugzeuge