Method for controlling an electrical deicing system
AssigneeAircelle
InventorsDavid Pereira, Laurence Lemains
Life of this patent
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Abstract
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.
Claims11
A method for commanding and controlling at least one resistive heating element belonging to an aircraft turbojet engine nacelle deicing set, comprising:
- obtaining, from a central control unit 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 to the resistive heating element.
Dependencies are inferred from the claim text.