Rotor type ground effect aircraft

The invention provides an aerovane type ground effect aircraft provided with spin wing of high rotational inertia. The invention is composed of main engine mounted on the middle top part of airframe, culvert propeller connected with the main engine by driving shaft, level short limbs of aerovane type ground effect aircraft mounted on the two sides of the airframe, short limb support buoy installed on the tip part of the short limb, air horizontal and vertical tail mounted on the rear end of the tail and submarine tail vane mounted at the undermost part of the rear end of the tail. An unpowered spin wing propeller composed of straight blade of multi-leaf length is mounted on the top of the airframe. A level short hydroflap is connected under the abdomen of the airframe. The spin swing affords above one-half of lift force of the aircraft, which can effectively increase the stability of the ground effect aircraft and anti-storm ability and instantaneous lift ability for flying across the obstacle with great use