System for Deicing and/or Defogging an Aircraft Surface, Method for Controlling Same, and Aircraft Equipped with Same

摘要

The invention concerns a system for deicing and/or defogging an aircraft surface ( 4 ) comprising: a temperature sensor ( 5 ) located proximate said surface ( 4 ) and adapted to generate a temperature information (TPT); a computer ( 20 ) adapted to generate a control information (CMD) based on the temperature information (TPT) and to transmit the control information (CMD) over a computer network ( 18 ) of the aircraft; an electric power supply system ( 8 ) located in the electrical center of the aircraft ( 18 ) and comprising a switch ( 12 ) adapted to be switched based on the control information (CMD); a heating element ( 6 ) located proximate said surface ( 4 ) and electrically powered via said switch ( 12 ). The invention also concerns a method for controlling such a system.