The invention discloses a tilting type electric vertical take-off and landing aircraft with foldable airfoils and an operation method. Comprising a
fuselage, a fixed section wing arranged on the
fuselage, a folding section wing connected to the fixed section wing through a wing folding
assembly, a vertical fin arranged at the
tail of the
fuselage, a fixed section horizontal
tail arranged on the vertical fin and a folding section horizontal
tail connected to the fixed section horizontal tail through a horizontal tail folding
assembly. The conversion of the aircraft among a folding mode, a helicopter mode and a fixed-wing aircraft mode can be realized under the action of the wing folding
assembly and the horizontal tail folding assembly, a front-end rotor wing is arranged on the fixed-section wing, a middle-end rotor wing is arranged on the folding-section wing, and a rear-end rotor wing is arranged on the folding-section horizontal tail. When the aircraft is parked on the ground, the folding section wings and the folding section horizontal tail can be folded, so that the
parking space needed by the aircraft is reduced, the requirement for special infrastructures is lowered, the cost is saved, the aircraft can be more easily integrated into the current limited space of a city, and the operation flexibility is enhanced.