A system for controlling icing on a surface of an aircraft, the system comprising: a carbon nanotube (CNT) heater, the CNT heater comprising: a CNT layer; a first encapsulation layer disposed on a first side of the CNT layer formed of a first encapsulation layer thermoplastic material; and a second encapsulation layer disposed on a second side of the CNT layer formed of a second encapsulation layer thermoplastic material. The system further includes a front composite structure comprising a front composite structure thermoplastic material disposed on a first side of the CNT heater; a rear composite structure comprising a rear composite structure thermoplastic material disposed on a first side of the CNT heater; and a sensor layer disposed between the CNT heater and one of the front composite structure and the rear composite structure.

    一种用于控制飞机的表面上的积冰的系统,所述系统包括:碳纳米管(CNT)加热器,所述CNT加热器包括:CNT层;第一封装层,所述第一封装层设置在由第一封装层热塑性材料形成的CNT层的第一侧上;以及第二封装层,所述第二封装层设置在由第二封装层热塑性材料形成的CNT层的第二侧上。所述系统还包括前复合结构,所述前复合结构包括设置在所述CNT加热器的第一侧上的前复合结构热塑性材料;后复合结构,所述后复合结构包括设置在所述CNT加热器的第一侧上的后复合结构热塑性材料;以及传感器层,所述传感器层设置在所述CNT加热器与所述前复合结构和所述后复合结构中的一者之间。


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    Titel :

    Integrated anti-icing system


    Weitere Titelangaben:

    一体式防冰系统


    Beteiligte:
    HEIN BERND (Autor:in) / SLANE CASEY (Autor:in) / WEBELOW JOHN MICHAEL (Autor:in) / BOTURA GALDEMIR CEZAR (Autor:in) / HAMMANN MARKUS (Autor:in)

    Erscheinungsdatum :

    21.04.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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