The invention relates to a flying
saucer type helicopter utilizing active
airflow to generate lifting power. As everyone knows, the asymmetric
airflow on the upper surfaces and lower surfaces of wings can generate lifting power, however for both a
fixed wing aircraft and a
propeller-driven aircraft, the wings move, the air is motionless, and
airflow is passively generated. According to the invention, an opposite approach is chosen. Specifically, the wings are fixed, actively generated airflow flows through the upper surfaces of the wings, an air
pressure difference is manufactured between the upper surfaces and lower surfaces of the wings so as to generate the lifting power, thus realizing a safe and simple aircraft that can achieve vertical take-off and landing, hovering,
level flight and pivot steering. The appearance of the aircraft is similar to a flying
saucer. By adjusting the angle between the airflow direction of the aircraft's upper surface and the radial direction, spin of the
fuselage can be controlled, and by adjusting the flow velocity distribution of the front, back, left and right directions, the inclination direction of the aircraft body can be changed to realize
level flight and direction control. The novel aircraft not only has all the advantages of traditional helicopters, but also has the characteristics of simplicity, compactness, safety, stability and the like, and is an
ideal solution to one-man aircrafts and unmanned reconnaissance aerial vehicles.