| 摘要 |
The present invention relates to a drone and a rotor blade structure of a drone and, more specifically, relates to a rotor blade structure having high thrust to transport a heavy object to maintain control efficiency along with structural stability and a drone having the same. According to the present invention, the rotor blade structure of a drone comprises a plurality of arms and propellers individually provided in the arms. Moreover, the number of the propellers individually provided in the arms is multiple. |
