An induction-heating system includes a susceptor located proximate to a flight surface of an aircraft. The susceptor comprises an array of wires arranged along a first axis. The array of wires is constructed of a ferromagnetic material having a selected Curie temperature. The induction-heating system also includes an electrically conductive coil including a plurality of coil windings oriented substantially perpendicular with respect to the first axis of the array of wires. The electrically conductive coil is configured to generate a magnetic field oriented substantially parallel with respect to the first axis of the array of wires. The electrically conductive coil is positioned to induce induction heating within the ferromagnetic material of the susceptor when the susceptor is below the selected Curie temperature.


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    Titel :

    INDUCTION-HEATING SYSTEM INCLUDING A SUSCEPTOR FOR GENERATING INDUCTION HEATING BELOW A SELECTED CURIE TEMPERATURE


    Beteiligte:
    HULL JOHN R (Autor:in) / BAUCUM JEFFREY PETER (Autor:in) / HENSON LANDON (Autor:in) / MATSEN MARC R (Autor:in)

    Erscheinungsdatum :

    10.11.2022


    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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    Bailey, E.L. | Engineering Index Backfile | 1936


    Induction heating

    Brown, D.W. | Engineering Index Backfile | 1953


    Induction heating

    Somes, H.E. | Engineering Index Backfile | 1946


    Induction heating

    Blasko, E. | Engineering Index Backfile | 1941


    INDUCTION HEATING SYSTEMS

    FRYSHMAN BERNARD | Europäisches Patentamt | 2020

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