The utility model belongs to the field of
airplane auxiliary dragging tools, and relates to an
airplane artificial leg design structure which comprises a main artificial leg and a
tail artificial leg. A main
landing gear of the aircraft is replaced by the main artificial leg, and a
tail landing gear of the aircraft is replaced by the
tail artificial leg; the main artificial leg comprises a frame, a movable wheel
assembly, a rotating wheel
assembly, an aircraft connecting
assembly, a steering device and a supporting assembly. The movable wheel assembly and the rotating wheel assembly are grounded, the frame is horizontally arranged above the movable wheel assembly and the rotating wheel assembly, and the supporting assembly and the steering device are connected among the movable wheel assembly, the rotating wheel assembly and the frame; the aircraft connecting assembly is connected to the upper portion of the frame and used for being connected with an aircraft
nose bracket. The problem of dragging the aircraft is solved, the aircraft body does not need to be transported to other places to be repaired, and the aircraft can be conveniently moved in a factory after the main artificial leg and the tail artificial leg are installed. The
airplane dragging device is simple in operation, easy in direction control when an airplane is dragged, large in rotating angle, labor-saving and high in dragging stability.