Provided is a flight device and a flight device control method that ensure safety even if a defect occurs in a power connection/disconnection unit. Rotor-side power transmission units 26 of a flight device 10 include first and second rotor-side power transmission units 261 and 262. Power connection/disconnection units 27 transmit power according to conditions and include first and second power connection/disconnection units 271 and 272. The first power connection/disconnection unit 271 is provided between a first engine-side power transmission unit 251 and the first rotor-side power transmission unit 261. The second power connection/disconnection unit 272 is provided between a second engine-side power transmission unit 252 and the second rotor-side power transmission unit 262. The arithmetic control unit 31 changes the flight status when the degree to which the first power connection/disconnection unit 271 transmits the power and the degree to which the second power connection/disconnection unit 272 transmits the power differ by a certain amount or more.


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    Title :

    FLIGHT DEVICE AND FLIGHT DEVICE CONTROL METHOD


    Additional title:

    FLUGVORRICHTUNG UND FLUGVORRICHTUNGSTEUERUNGSVERFAHREN
    DISPOSITIF DE VOL ET PROCÉDÉ DE COMMANDE DE DISPOSITIF DE VOL


    Contributors:

    Publication date :

    2025-02-05


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge / B64U



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