The embodiment of the invention discloses an aircraft which comprises a fuselage, an engine as well as a front end air hole, a tail air hole, a left side air hole, a right air hole, an upper air hole and a lower air hole which are respectively arranged at the front, at the rear, at the left, at the right, at the upper and at the lower of the fuselage, wherein all the air holes are provided with air valves; and the aircraft also comprises air pipes used for connecting the engine and the air holes, and a controlled used for respectively controlling the flow rate of the air flow in all the air valves. The aircraft utilizes the controller to control the opening and closing of the air valves so as to control air to pass in and out the air holes, thus regulating the work and the power of the engine, reaching the requirements of different elevating forces and thrusts needed by various flight attitudes, and realizing the flight attitudes such as vertical lifting, horizontal flight, hovering, turning and the like of the aircraft. The aircraft can vertically lift in a narrow place, and improves the motility of the aircraft so as to lead the aircraft to move rapidly. The aircraft has low manufacturing and using costs, easy operation, low noise, safety and reliability.