The invention relates to a vertical
takeoff and landing
fixed wing unmanned aerial vehicle with variable
pitch propellers. The vertical
takeoff and landing
fixed wing unmanned aerial vehicle comprises an unmanned aerial vehicle body, wherein wings are separately and fixedly mounted at the middle part of the unmanned aerial vehicle body, and
tail wings are separately and fixedly mounted at the
tail of the unmanned aerial vehicle body; an engine is mounted at the head of the unmanned aerial vehicle body; two sets of variable
pitch propellers are mounted on an output shaft of the engine; when the unmanned aerial vehicle runs, the rotating directions of the two sets of the variable
pitch propellers are opposite; each buffer lifting mechanism is arranged on the corresponding
tail wing, and comprises a connecting rod, a buffering device and a roller, wherein one end of each connecting rod is hinged to the corresponding tail wing, and the other end of the connecting rod is hinged to the corresponding roller; the middle part of each connecting rod is hinged to the corresponding buffering device which is fixedly mounted in the corresponding tail wing; vertical
takeoff, landing and parking are performed by the buffer lifting mechanisms, so that on one hand, the vertical
takeoff and landing fixed wing unmanned aerial vehicle has the
flight speed of a fixed wing unmanned aerial vehicle, and on the other hand, can perform vertical takeoff, landing and hanging like a rotor unmanned aerial vehicle, and the dependency of the unmanned aerial vehicle on site runways is greatly reduced; and rollers are separately arranged at the tail wings of the unmanned aerial vehicle, and in the
flight process, the rollers are driven by an
air current to rotate at a high speed, so that in the
flight process, the attitude of the unmanned aerial vehicle has better stability.