The invention discloses a fast-assembling mechanism for wings of an unmanned aerial vehicle. The fast-assembling mechanism comprises a frame, a button, a button shell, a button spring, a button base,a button center, a fixing block, a thick carbon tube, a spring pin seat, a spring pin, a pin spring, a spring pin shell, a thin carbon tube, the inner segment wing and the outer segment wing. The outer segment wing is arranged on one side of the inner segment wing, the frame is arranged in the middle of the inner segment wing, and the button is arranged in the middle of the frame. The thick carbontube is arranged on one side of the frame, and the thin carbon tube is arranged on the other side of the frame. The fixing block is arranged at the top end of the thick carbon tube, and the button center is arranged at the top end of the fixing block. The button shell is arranged at the top end of the button center and internally provided with the button spring, and the button base is arranged atthe bottom end of the button shell. The wings are mounted through the spring pin, and when the outer segment wing is inserted and pulled, a pin or a screw does not need to be assembled; the fast-assembling mechanism adopts modular design, so that the mechanism is easier to repair and replace; and assembly and disassembly of the wings are convenient, no tool is needed, and out-field operation is facilitated.