복합 구조물은 매트릭스 재료와, 그리고 섬유 재료에 주입된 다수의 탄소 나노튜브(CNTs)를 포함하는 탄소 나노튜브(CNT)-주입 섬유 재료를 포함한다. 상기 CNT-주입 섬유 재료는 매트릭스 재료의 일부에 걸쳐 배치된다. 상기 복합 구조물은 CNT-주입 섬유 재료를 통해 전류의 적용에 맞게 적응되어 복합 구조물의 가열을 제공한다. 발열체는 섬유 재료에 주입된 다수의 CNTs를 포함하는 CNT-주입 섬유 재료를 포함한다. 상기 CNT-주입 섬유 재료는 이를 필요로 하는 구조물에 가열을 제공하기에 충분한 비율로 존재한다.

    A composite structure includes a matrix material and a carbon nanotube (CNT)-infused fiber material that includes a plurality of carbon nanotubes (CNTs) infused to a fiber material. The CNT-infused fiber material is disposed throughout a portion of the matrix material. The composite structure is adapted for application of a current through the CNT-infused fiber material to provide heating of the composite structure. A heating element includes a CNT-infused fiber material includes a plurality of CNTs infused to a fiber material. The CNT-infused fiber material is of sufficient proportions to provide heating to a structure in need thereof.


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    Titel :

    CNT-BASED RESISTIVE HEATING FOR DEICING COMPOSITE STRUCTURES


    Weitere Titelangaben:

    복합 구조물 제빙을 위한 CNT계 저항 가열


    Erscheinungsdatum :

    13.01.2017


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Koreanisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / H05B ELECTRIC HEATING , Elektrische Heizung



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