A device for emergency disconnection of a high voltage electrical connection between a power source and a high voltage component of an electric aircraft in response to a crash. The device includes a controller, where the controller is configured to receive a sensor datum from a sensor of device, to determine a crash element between and initiate a disconnection protocol as a function of the crash element.
Emergency high voltage disconnection device for an electric aircraft
24.06.2025
Patent
Elektronische Ressource
Englisch
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