▎ 摘　　要

NOVELTY - The composite structure has a protective layer (1), graphene modified quartz fibre heating component (2) and a bearing layer (3). The bearing layer is paved on the mold. Graphene modified quartz fibre heating component is paved on the bearing layer. The graphene of the modified quartz fibre heating component is paved with a protective layer. Graphene the modified quartz fibre heating component is composed of a graphene heating fabric and an electrode, and the electrodes are arranged on two sides of the graphene heating fabric USE - Wave-transparent anti-icing composite structure for use in an aircraft. ADVANTAGE - The anti-icing design of the integrated antenna area of the front edge of the unmanned aerial vehicle is compatible with the wave transmission requirement and the anti-deicing requirement, and it has good feasibility and manufacturability. The composite structure is capable of satisfying high frequency antenna frequency band (X wave band and more), at the same time thus it realizes anti-ice function after electrifying and heating. DESCRIPTION OF DRAWING(S) - The drawing shows a schematic diagram of the wave-transmitting and anti-deicing function composite structure. (Drawing includes non-English language text) 1Protective layer 2Graphene modified quartz fibre heating component 3Bearing layer