De-icing and/or anti-icing system for the leading edge of an...

B - Operations – Transporting – 64 – D

Patent

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B64D 15/12 (2006.01)

Patent

CA 2721365

The invention relates to a de-icing and/or anti-icing system for the leading edge of an aircraft wing or for the lip (1) of the air intake of an aircraft engine, characterised in that it includes a plurality of infrared emitting members (13) arranged inside said leading edge or said lip (1), power supply means (17) for said emitters (13), and means (27) for controlling said power supply means (17).

Ce système de dégivrage et/ou d'antigivrage pour bord d'attaque de voilure d'aéronef ou pour lèvre (1) d'entrée d'air de moteur d'aéronef, est remarquable en ce qu'il comprend une pluralité d'émetteurs infrarouges (13) disposés à l'intérieur dudit bord d'attaque ou de ladite lèvre (1), des moyens (17) d'alimentation électrique de ces émetteurs (13), et des moyens (27) de commande de ces moyens d'alimentation électrique (17).

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