Abstract: A system and method for anti-icing and de-icing an aircraft are provided. The system includes an electrically conductive coating, an electrical circuit having one or more electrical leads, a control unit, a plurality of temperature sensors connected to the control unit, and a plurality of ice detector sensors connected to the plurality of temperature sensors and the control unit. A process for anti-icing and de-icing an aircraft is also provided that includes applying electrically conductive coating under the skin of an airplane surface and attaching electrical wiring or metal strips to the skin of the airplane surface, and directing electricity to the electrical wiring or metal strips.

Abstract: Embodiments for a system and method for anti-icing and de-icing an aircraft are provided. The system includes an electrically conductive coating, an electrical circuit having one or more electrical leads, a control unit, a plurality of temperature sensors connected to the control unit, and a plurality of ice detector sensors connected to the plurality of temperature sensors and the control unit. A process for anti-icing and de-icing an aircraft is also provided that includes applying electrically conductive coating under the skin of an airplane surface and attaching electrical wiring or metal strips to the skin of the airplane surface, and directing electricity to the electrical wiring or metal strips.