An aircraft ice protection system includes a heating substrate with a coating in intimate thermal contact with the heating substrate. The thermal effusivities of the heating substrate and the coating are different from one another for interference of thermal waves reflected from the coating with thermal waves generated in the heating substrate. A pulse generator can be operatively connected to the heating substrate to convert pulsed electrical power from the pulse generator into thermal energy for ice removal or prevention.


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    Title :

    Pulsed electrothermal ice protection systems with coated heating substrates


    Contributors:

    Publication date :

    2019-07-23


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    H05B ELECTRIC HEATING , Elektrische Heizung / B60L PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES , Antrieb von elektrisch angetriebenen Fahrzeugen / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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