The invention discloses a carbon fiber composite material plate with a deicing structure, which comprises a carbon fiber bottom plate, a carbon fiber cover and a heating plate, the opposite sides of the carbon fiber bottom plate and the carbon fiber cover are both provided with protective layers, the inner groove wall of the carbon fiber bottom plate is buckled and connected with two connecting tables, and the two ends of the heating plate are both fixedly connected with connecting blocks. And connecting grooves are formed in the opposite sides of the two connecting tables correspondingly, the connecting blocks are connected with the connecting grooves in a meshed mode, and heating pipes are arranged in inner grooves of the heating plates, and the technical field of aeronautical materials is related to the beneficial effects that a heating structure is arranged in the empennage carbon fiber composite material plate, and a graphene heat conduction layer with the high heat conduction performance is matched, so that the heat conduction performance of the empennage carbon fiber composite material plate is improved; therefore, when the empennage is iced, the effect of heating and deicing can be achieved in time, and the deicing efficiency is further improved through the heat conduction effect of graphene.
本发明公开了一种带有除冰结构的炭纤维复合材料板,包括碳纤维底板、碳纤维盖和加热板,碳纤维底板和碳纤维盖相反的一侧均设有防护层,碳纤维底板内槽壁扣接连接有两个连接台,加热板两端均固定连接有连接块,两个连接台相对一侧均开设有连接槽,连接块与连接槽啮合连接,加热板内槽设有加热管,涉及航空材料技术领域,本发明的有益效果:通过在尾翼碳纤维复合材料板内部设置加热结构,配合导热性能较强的石墨烯导热层,进而能够在尾翼出现结冰状况时,及时的进行加热除冰的效果,并且通过石墨烯的导热效果,进一步提升除冰的效率。
Carbon fiber composite material plate with deicing structure
一种带有除冰结构的炭纤维复合材料板
2023-03-03
Patent
Electronic Resource
Chinese
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