System for deicing and/or defogging an aircraft surface,...

Details System for deicing and/or defogging an aircraft surface,... System for deicing and/or defogging an aircraft surface,...

B - Operations, Transporting

64

D

B64D 15/12 (2006.01) B64D 15/22 (2006.01)

Patent

CA 2623320

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.

Un système de dégivrage et/ou de désembuage d'une surface (4) d'un aéronef comprend : - un capteur de température (5) situé à proximité de ladite surface (4) et apte à générer une information de température (TPT) ; - un calculateur (20) apte à générer une information de commande (CMD) à partir de l'information de température (TPT) et à émettre l'information de commande (CMD) sur un réseau informatique (18) de l'aéronef ; - un système d'alimentation électrique (8) situé dans le cAEur électrique de l'aéronef, apte à recevoir l'information de commande (CMD) sur le réseau informatique (18) et comprenant un interrupteur (12) apte à être commuté en fonction de l'information de commande (CMD) ; - un élément chauffant (6) situé à proximité de ladite surface (4) et alimenté électriquement à travers ledit interrupteur (12). Un procédé de commande d'un tel système est également proposé.

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