The invention relates to a wing folding mechanism for an unmanned plane. The wing folding mechanism comprises a first sleeve, a second sleeve, a support shaft, a locking part, a tractive part and a connecting rod, wherein the first sleeve is provided with a first cavity; the second sleeve is provided with a second cavity; the support shaft is arranged in the first cavity in a slidable manner; the locking part is mounted on the side face of the first sleeve and has a locking state and an unlocking state; the tractive part is fixed in the second cavity and can move back and forth in the shaft axis direction of the first sleeve; the connecting rod is used for connecting the support shaft and the tractive part; the wing folding mechanism has an unfolding state and a folding state. On one aspect, part of the folding mechanism enters the support shaft of the second cavity, so that the folding mechanism is in the unfolding state; on the other aspect, under the action of the tractive part, the connecting rod enables the first sleeve to rotate relative to the end face of the second sleeve, so that the folding mechanism is in the folding state, as a result, both the unfolding and folding states are realized without a wheel gear serving as a transmission part; in addition, the wing folding mechanism is compact in structure and stable in motion, and few requirements are required for the torque of a motor.