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.
FLIGHT DEVICE AND FLIGHT DEVICE CONTROL METHOD
FLUGVORRICHTUNG UND FLUGVORRICHTUNGSTEUERUNGSVERFAHREN
DISPOSITIF DE VOL ET PROCÉDÉ DE COMMANDE DE DISPOSITIF DE VOL
2025-02-05
Patent
Electronic Resource
English
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