▎ 摘　　要

NOVELTY - The plate has a protective layer (4) that is provided on the opposite side of a carbon fiber bottom plate (1) and a carbon fiber cover (2). The carbon fiber bottom plate is buckled and connected with the connecting platforms (5) on the inner groove wall. Both ends of the heating plate (3) are fixedly connected with connecting blocks (6). The opposite sides of the two connecting platforms are provided with connecting grooves. The connecting block is meshed with the connecting groove. A heating pipe (7) is provided in the inner groove of the heating plate. USE - Carbon fiber composite panel with deicing structure for manufacturing aerospace and aviation equipment. ADVANTAGE - The plate is provided with a heating structure in the tail wing carbon fiber composite material plate, matched with the heat conducting graphene of a heat conducting layer, so as to empennage icing condition, timely heating and de-icing effect, and through heat conducting effect of graphene, thus improving efficiency of deicing. The plate allows a detachable carbon fiber plate and a modularized heating structure to be convenient for subsequent maintenance and replacement, so that use is more flexible. DESCRIPTION OF DRAWING(S) - The drawing shows a front sectional view of the carbon fiber composite material plate with de-icing structure. 1Carbon fiber bottom plate 2Carbon fiber cover 3Heating plate 4Protective layer 6Connecting block 7Heating pipe 13Insulating pressing plate