The invention provides a fiber composite component, a component system, an aircraft, and application. The component comprises a plurality of layers of fibers embedded in a matrix material, further comprising at least two rupture sensing fibers arranged on or in at least one of the layers, wherein the rupture sensing fibers are carbon fibers having an electrically insulating coating, and the component comprises two electrical connection devices, each being accessible from an outer delimiting surface or an outer edge of the component, wherein the electrical connection devices are connected to different ends of the rupture sensing fibers.

    提出了一种纤维复合材料部件、部件系统、飞行器和用途。所述部件包括嵌入基体材料中的纤维的多个层,进一步包括至少两个布置在所述层中的至少一个层中或上的断裂感测纤维,其中,所述断裂感测纤维是具有电绝缘涂层的碳纤维,并且其中,所述部件包括两个电连接装置,每个电连接装置均可从所述部件的外分界表面或外缘触及,其中,所述电连接装置连接至所述断裂感测纤维的不同端部。


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    Title :

    Fiber composite component, component system, aircraft, and application


    Additional title:

    纤维复合材料部件、部件系统、飞行器和用途


    Contributors:
    LINDE PETER (author) / ASP LEIF (author) / ZENKERT DAN (author)

    Publication date :

    2020-06-30


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    G01D MEASURING NOT SPECIALLY ADAPTED FOR A SPECIFIC VARIABLE , Anzeigen oder Aufzeichnen in Verbindung mit Messen allgemein / B64C AEROPLANES , Flugzeuge / G01N Untersuchen oder Analysieren von Stoffen durch Bestimmen ihrer chemischen oder physikalischen Eigenschaften , INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES



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