A flow body for an aircraft includes a skin having a first flow surface, the first flow surface including a flow-affecting section, the flow-affecting section including: at least one first layer including a first fiber composite material; at least one separator layer; at least one third layer comprising a third fiber composite material; and at least one base layer comprising a base fiber composite material wherein the first layer comprises lithiated carbon fibers embedded in a matrix to form a negative electrode wherein the third layer comprises carbon fibers having an electrode active material coating to form a positive electrode wherein the separator layer comprises a non-conductive material, the non-conductive material is used for electrically isolating the first layer and the third layer from each other; the flow affecting section is configured to selectively raise a region of an arrangement of the first layer, the separator layer, and the third layer from the base layer upon application of a voltage between the first layer and the third layer to form a protrusion on the flow body.

    一种用于飞行器的流动本体包括具有第一流动表面的蒙皮,所述第一流动表面包括流动影响区段,所述流动影响区段包括:至少一个第一层,所述至少一个第一层包括第一纤维复合材料;至少一个分隔物层;至少一个第三层,所述至少一个第三层包括第三纤维复合材料;以及至少一个基层,所述至少一个基层包括基础纤维复合材料,其中,所述第一层包括包埋在基质中的锂化碳纤维以形成负电极,其中,所述第三层包括具有电极活性材料涂层的碳纤维以形成正电极,其中,所述分隔物层包括非导电材料,所述非导电材料用于使所述第一层与所述第三层彼此电隔离,并且其中,所述流动影响区段被配置成在所述第一层与所述第三层之间施加电压时选择性地使由第一层、分隔物层和第三层构成的布置的区域从所述基层升高以在所述流动本体上形成凸起。


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    Titel :

    FLOW BODY FOR AIRCRAFT WITH SELECTIVELY ACTIVABLE SWAVE


    Weitere Titelangaben:

    用于飞行器的具有可选择性地启用的激波凸起的流动本体


    Beteiligte:
    LINDE PETER (Autor:in) / MAJONZA WOLFGANG (Autor:in)

    Erscheinungsdatum :

    2022-06-21


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / F03G Feder-, Gewichts-, Trägheits- oder ähnliche Kraftmaschinen , SPRING, WEIGHT, INERTIA, OR LIKE MOTORS



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