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.
Electric vertical takeoff and landing aircraft and control device for electric vertical takeoff and landing aircraft
2025-04-15
Patent
Electronic Resource
English
European Patent Office | 2021
|European Patent Office | 2021
|European Patent Office | 2022
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