The application provides a
propeller rectification structure and a vertical take-off and landing fixed-wing unmanned aerial vehicle, and belongs to the technical field of unmanned aerial vehicles. The
propeller rectification structure comprises a
cantilever, the two ends of the
cantilever are respectively provided with motors, the output ends of the motors are provided with double-blade propellers, the two ends of the
cantilever are respectively movably connected with rectification covers, a driving mechanism is arranged in the cantilever to drive the rectification covers to move up and down, the rectification covers movably cover the corresponding propellers, and an angle detection mechanism is arranged in the cantilever to detect the rotation angle of the
propeller. The application has the following effects: the rectification cover is arranged at the upper end of the propeller, the driving mechanism drives the rectification cover to move away from the propeller during vertical take-off and landing, the angle detection mechanism is matched with the motor to align the double-blade propeller with the rectification cover during
level flight and cruising, and then the driving mechanism drives the rectification cover to cover the propeller, so that the rectification of the propeller is realized, the
level flight resistance is reduced, and the
flight stability is improved.