SYSTEM FOR DEICING AND/OR DEFOGGING AN AIRCRAFT SURFACE, METHOD FOR CONTROLLING SUCH A SYSTEM, AND AIRCRAFT EQUIPPED WITH SUCH A SYSTEM

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.