The invention relates to a ducted coaxial twin-screw unmanned aerial vehicle, comprising a power
system, a
bevel gear transmission system, a control plane regulating
system and a rack, wherein the power
system comprises three transmission shafts, a motor and a core frame; the
bevel gear transmission system comprises upper and lower internal
bevel gear disks, a plane pushing bearing, a blade mounting clip, blades and an internal duct; and the control plane regulating system comprises a control plane mounting clip, a bearing, a control plane retaining clip, a steering engine draw rod retaining clip, a steering engine draw rod, a
servo steering engine and a steering engine arm. The ducted coaxial twin-screw unmanned aerial vehicle disclosed by the invention has the following beneficial effects that: 1, through the ducted mode, the efficiency of the blades is greatly improved; 2, through the bevel
gear transmission system, the effective efficiency of the motor is maximally exerted; 3, through the coaxial twin-screw mode, lifting power can be supplied more efficiently; and 4, through controlling the aircraft attitude in multiple control planes, the unmanned aerial vehicle is more stable.