Method for controlling an electrical deicing system

Details Method for controlling an electrical deicing system Method for controlling an electrical deicing system

B - Operations, Transporting

64

D

B64D 15/12 (2006.01) B64D 15/20 (2006.01)

Patent

CA 2741457

The present invention relates to a method for commanding and controlling at least one resistive heating element (1) belonging to an aircraft turbojet engine nacelle deicing set, characterized in that it involves the steps aimed at: obtaining, from a central control unit (6) of the aircraft, parameters representative of the exterior flight conditions; determining a thermal model corresponding to the flight conditions obtained; as a function of the thermal model, delivering the appropriate corresponding electrical power (4) to the resistive heating element.

La présente invention se rapporte à un procédé de contrôle et de commande d'au moins une résistance chauffante (1) appartenant à un ensemble de dégivrage d'une nacelle de turboréacteur d'un avion, caractérisé en ce qu'il comprend les étapes visant à : obtenir d'une unité centrale de contrôle (6) de l'avion des paramètres représentatifs des conditions extérieures de vol; déterminer un modèle thermique correspondant aux conditions de vol obtenues; en fonction du modèle thermique délivrer à la résistance chauffante la puissance électrique (4) correspondante appropriée.

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