The present invention relates to a land-water-air three-purpose rotor aircraft, which comprises a body, a cabin cover, buoys, wheels, support rods, screw propellers and a motor, wherein the cabin cover is arranged on the body, a cabinet is formed between the cabin cover and the body, the buoys are arranged on both sides of the body, the wheels are arranged below the buoys and can be shrunk into the buoys, four groups of the screw propellers are arranged and are respectively arranged on the front ends and the rear ends of both sides of the body through the four support rods, the motor separately drives the four groups of the screw propellers to rotate, the support rod is a foldable rod, and the screw propellers are positioned at different positions when the support rods are folded. Compared to the aircraft in the prior art, the aircraft of the present invention achieves the applications in the three fields of land, water and air, has the multi-function, has advantages of simple structure arrangement and easy control, and further has advantages of substantially reduced cost, high running stability and high safety compared to other aircrafts.