▎ 摘　　要

NOVELTY - The structure has a micro-strip antenna layer (2) provided with a graphene pattern layer (21) and a micro-strip substrate layer (22). A composite material supporting layer (1) is glued on a surface of pattern layer graphene. The micro-strip substrate layer is adhered with a bottom surface of pattern layer graphene through first adhesive (5). An ethylene TFE (ETFE) film layer (3) is adhered with a bottom surface of the micro- strip substrate layer by second adhesive (6). The graphene pattern layer is provided with multiple graphene micro-strip units that are welded together by a copper welding sheet to form a conductive path. The graphene micro-strip unit is etched with a hollow circuit pattern. USE - Graphene film conformal antenna structure for use as an unmanned aerial vehicle wing in military, agriculture and disaster relief fields. ADVANTAGE - The structure has light weight, high manufacturing efficiency, better toughness and high strength, and can independently forme a wing-shaped surface, so that ensures flight wing and radar detection function, reduce total weight of an unmanned aerial vehicle load in an assembling mode so as to save a space of an aerial vehicle, improve radar function for loading an electronic device, ensure better assembling form so as to reduce vehicle energy consumption, thus improving endurance ability, realize tight connection between layer structures and simplify manufacturing process. DETAILED DESCRIPTION - An INDEPENDENT CLAIM is also included for a graphene film conformal antenna structure manufacturing method. DESCRIPTION OF DRAWING(S) - The drawing shows a schematic view of the graphene film conformal antenna structure. 1Composite material supporting layer 2Micro-strip antenna layer 3ETFE film layer 5First adhesive 6Second adhesive 21Graphene pattern layer 22Micro-strip substrate layer