A controller (a control unit) of a power supply system of a vertical take-off and landing aircraft is configured to: after lift is generated by wings (a front wing and a rear wing), perform stop control of controlling electric power supplied to a motor so that rotation of a VTOL rotor continues to stop; temporarily cancel the stop control in response to the temperature of any one switching element detected by a temperature detection unit (a temperature sensor) becoming equal to or higher than a temperature threshold during the stop control; and resume the stop control after the stop control has been temporarily canceled.


    Access

    Download


    Export, share and cite



    Title :

    Power supply system of vertical take-off and landing aircraft


    Contributors:

    Publication date :

    2025-08-05


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B60L PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES , Antrieb von elektrisch angetriebenen Fahrzeugen



    VERTICAL TAKE-OFF AND LANDING AIRCRAFT POWER SUPPLY SYSTEM

    ATAMANOV ALEKSANDR VIKTOROVICH | European Patent Office | 2020

    Free access

    POWER SUPPLY SYSTEM OF VERTICAL TAKE-OFF AND LANDING AIRCRAFT

    YOSHIMURA KAISAKU / AIZAWA BON / UCHIDA KENTA et al. | European Patent Office | 2024

    Free access

    POWER SUPPLY SYSTEM OF VERTICAL TAKE-OFF AND LANDING AIRCRAFT

    YOSHIMURA KAISAKU / AIZAWA BON / UCHIDA KENTA et al. | European Patent Office | 2024

    Free access