Abstract: An electric aircraft is capable of vertically taking off and landing. The aircraft includes a fuselage, front and rear power units, power pods, main wings, ailerons, front landing gears, a tail wing and a rear landing gear. The power units include first and second electric duct groups. The first electric duct group includes two electric duct fans symmetrically and connected to two sides of a front portion of the fuselage respectively. The second electric duct group includes two electric duct fans symmetrically provided at two sides of a rear portion of the fuselage respectively. The power pods are configured to connect the fuselage to the first electric duct group. The two main wings are symmetrically and foldably connected to two sides of the fuselage respectively. The two ailerons are symmetrically connected to front ends of the two main wings respectively.

Abstract: The present disclosure belongs to the technical field of flight vehicle power devices, and particularly relates to a novel electric driving force device. More than two sets of driving motors are distributed in a solar planetary manner on a radial spatial plane with an output shaft as a center of gyration, to drive more than one set of reducing mechanism in parallel, so as to provide electric driving power for a flight vehicle.