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INTEGRATED LIGHTNING PROTECTION AND ELECTRICAL DE-ICING FOR AERODYNAMIC STRUCTURES

机译:航空结构的综合防雷和电气除冰

摘要

An example method includes: forming a conductive layer on at least a portion of a surface of a substrate, where the substrate comprises a composite material of an aerodynamic structure, and where the conductive layer is configured to provide a conductive path to conduct an electric current generated by a lightning strike to an electrically-grounded location; depositing an insulating layer on the conductive layer; removing one or more portions of the insulating layer to form respective gaps in the insulating layer and expose corresponding one or more portions of the conductive layer; and forming a resistive-heater layer on the insulating layer such that the resistive-heater layer fills the respective gaps in the insulating layer and contacts the corresponding one or more portions of the conductive layer, such that when electric power is provided to the conductive layer, the electric power is communicated to the resistive-heater layer thereby generating heat therefrom. (Fig. 12)
机译:一种示例方法包括:在衬底的表面的至少一部分上形成导电层,其中该衬底包括空气动力学结构的复合材料,并且其中该导电层被配置为提供导电路径以传导电流。雷击产生的接地点;在导电层上沉积绝缘层;去除绝缘层的一个或多个部分,以在绝缘层中形成各自的间隙,并暴露出导电层的相应的一个或多个部分;在绝缘层上形成电阻加热器层,以使电阻加热器层填充绝缘层中的各个间隙并接触导电层的相应的一个或多个部分,从而在向导电层提供电力时之后,电力被传送到电阻加热器层,从而从其产生热量。 (图12)

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