An ice protection system for an aircraft component includes a plurality of heaters. The aircraft component has at least two section and a junction area. At least one of the heaters is an H-shape carbon allotrope heater designed to apply heat to the junction area and prevent ice accumulation in the junction area.


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    Titel :

    HEATER DESIGN FOR CARBON ALLOTROPE ICE PROTECTION SYSTEMS


    Beteiligte:
    SLANE CASEY (Autor:in) / HU JIN (Autor:in) / CHING NATHANIEL (Autor:in) / BOTURA GALDEMIR CEZAR (Autor:in) / MULLEN JAMES A (Autor:in) / DIDYK MARK JAMES (Autor:in)

    Erscheinungsdatum :

    18.04.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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