The invention relates to an unmanned aerial vehicle, in particular to a military unmanned aerial vehicle with portable united wings. According to the military unmanned aerial vehicle with portable united wings, a wing stiffener and a sliding block are arranged on a fuselage, a propeller is arranged at the tail end of the fuselage, and a vertical tail is arranged at the tail end of the fuselage; one end of the front wing is hinged to the wing stiffener, and the other end of the front wing is hinged to one end of a rear wing; the other end of the rear wing is hinged to the sliding block; the sliding block slides along the tail end of the fuselage to one side close to the wing stiffener, so that the wings are driven to be close to the fuselage; the vertical tail is hinged to the fuselage, and can be levelly put at the tail end of the fuselage or perpendicular to tail end of the fuselage. According to the military unmanned aerial vehicle with portable united wings provided by the invention, the portability of a multiple-spindle aircraft and favorable flight performance of a fixed wing aircraft are fully used. The unmanned aerial vehicle is put in a knapsack after being folded, so that the unmanned aerial vehicle is convenient to carry, and the portability that the unmanned aerial vehicle is easy to carry is fully reflected. Before flight, the unmanned aerial vehicle is taken out from the knapsack, the unmanned aerial vehicle is thrown manually to fly, and in the manual throwing process, the wings and the vertical tails are ejected to be in the flight state, and land in the sliding manner.