A device for defrosting / modular anti-icing of a surface aerodynamic.

摘要

The present invention relates to a device for de-icing / de-icing of the wing of an aircraft comprising at least an aerodynamic surface, for example a blade of a rotorcraft or an aircraft wing, this aerodynamic surface being provided with a plurality of heating elements 54.de addition, at least two heating elements 54 are electrically powered by a single electrical power supply means 1.