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 aircraftsurface (4) comprising: a temperature sensor (5) located proximate saidsurface (4) and adapted to generate a temperature information (TPT); acomputer (20) adapted to generate a control information (CMD) based on thetemperature 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 aswitch (12) adapted to be switched based on the control information (CMD); aheating element (6) located proximate said surface (4) and electricallypowered via said switch (12). The invention also concerns a method forcontrolling such a system.