| 摘要 |
PROBLEM TO BE SOLVED: To reduce the weight of an electric aircraft.SOLUTION: The present invention provides an electric aircraft comprising a plurality of rotary wings, a motor that rotates each of the rotary wings, a support shaft that supports each rotary wing and motor, a motor control unit that controls the rotation of each motor, a plurality of power supply lines that supply each pair of motors with power, and a plurality of battery modules each connected to a power supply line.SELECTED DRAWING: Figure 5 |
