This project is a prototype developed jointly by the Aviation Industry Helicopter Design Institute and Jingdezhen Tianyi Aviation Technology Co., Ltd. The maglev rotor unmanned aerial vehicle is electrically driven and remotely controlled for flight. It has flight functions such as vertical takeoff and landing, forward flight, hovering, and yaw. During fast forward flight, the tail culvert can tilt forward to provide thrust, and the main lift is generated by the wings.


Main technical parameters:


Wing span: 1550mm


Captain: 1330mm


Main culvert diameter: 480mm


Tail culvert diameter: 120mm


Maximum takeoff weight: 12kg


Battery life: 20 minutes