飞机石墨烯电热组件构型设计及除冰性能实验研究
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中国民用航空飞行学院,广汉 618307

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TB33/V25

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基于流体定向导流的零能耗飞机防除冰研究(PHD2023-008);民航局教育人才类项目(MHJY2023051);中国民用航空飞行学院博士创新能力提升计划项目(PHD2023-008)


Experimental Study on Configuration Design and Deicing Performance of Aircraft Graphene Electric Heating Component
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Civil Aviation Flight University of China,Guanghan 618307

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    摘要:

    为获取具备高效节能、优良导电与导热性能的电热组件构型,选取具备协同效应的石墨烯(Gr)与碳纳米管(CNTs)两种材料,运用标准喷涂法制备带有图案的电热涂层,并基于该涂层设计电热除冰装置。采用碳化后的导电油性石墨烯(CNT-GO,Carbon Nanotube-Graphene Oxide)开展涂层制备工作,借助扫描电子显微镜对该涂层的微观形貌进行分析,从微观层面揭示其电热性能变化的内在机理。同时,在自行搭建的除冰实验台上,对除冰装置样件的电热升温性能和除冰性能进行测试。研究结果显示,井字形发热涂层的温升速率更快,且表面温度均匀性更佳。基于此新型涂层的电热除冰装置结构简洁,易于与飞机表面结合,其在电热过程中产生的平均温度能够有效加速冰层融化,证实了该构型设计在降低电热除冰能耗方面的可行性。

    Abstract:

    To obtain an electrothermal component configuration with high efficiency, energy conservation, and excellent electrical and thermal conductivity,two materials-graphene (Gr) and carbon nanotubes (CNTs)-that exhibited a synergistic effect were selected.A standard spraying method was adopted to prepare patterned electrothermal coatings, and an electrothermal deicing device was designed based on these coatings.Carbonized conductive oil-based CNT-GO(Carbon nanotube-graphene oxide) was used for coating preparation.Scanning electron microscopy (SEM) was employed to analyze the microscopic morphology of the coating,revealing the internal mechanism underlying the changes in its electrothermal properties at the microscale.Meanwhile,tests on the electrothermal heating performance and deicing performance of the deicing device prototype were conducted on a self-built deicing experimental bench.The results show that the grid-shaped heating coating has a faster temperature rise rate and better surface temperature uniformity.The electrothermal deicing device based on this new type of coating features a simple structure and can be easily integrated with aircraft surfaces.The average temperature generated during its electrothermal process can effectively accelerate ice melting,which verifies the feasibility of this configuration design in reducing the energy consumption of electrothermal deicing.

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引用本文

庞杰,谢磊,王晓鹏,岳越.飞机石墨烯电热组件构型设计及除冰性能实验研究[J].宇航材料工艺,2026,56(1):72-78.

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  • 收稿日期:2023-07-23
  • 最后修改日期:2023-10-08
  • 录用日期:2023-10-08
  • 在线发布日期: 2026-02-28
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