▎ 摘　　要

NOVELTY - The system has a lead electrode (1), a wing-shaped electrode (2), an insulating frame (5) and a high voltage power supply. The wing-shaped electrode is fixed on the insulating frame. The lead electrode and the wing-shaped electrode are arranged in parallel at intervals. The lead electrode and the wing-shaped electrode are coated with graphene. The lead electrode is connected with a high voltage anode output end of the high voltage power supply. The wing-shaped electrode is connected with a high voltage cathode output end of the high voltage power supply. A number of the lead electrode and the wing-shaped electrode is same and not less than 2. The wing-shaped electrode is NACA0010 shaped aluminium foil polymethacrylimide foam. USE - Lead-wing type electrode ion wind solid propulsion system for small micro aircraft. ADVANTAGE - The lead-wing type electrode ion wind solid propulsion system includes simple structure, simple preparation, convenient for later maintenance, and includes low working noise, low carbon discharge and large output thrust, and suitable for small micro aircraft. DESCRIPTION OF DRAWING(S) - The drawing shows a structure schematic diagram of a lead-wing type electrode ion wind solid propulsion system. Lead electrode (1) Wing-shaped electrode (2) Fixing plate (3) Insulating bracket (4) Insulating frame (5)