Energy-efficient electro-thermal ice-protection system

B - Operations – Transporting – 64 – D

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B64D 15/12 (2006.01) B64D 15/16 (2006.01)

Patent

CA 2615166

A region of an airfoil to be protected from accreted ice is heated to reduce the strength of the bond between the ice and the airfoil, and is mechanically deformed to shed the accreted ice after the bond has been sufficiently weakened. Heating ceases before substantial water runback is generated. The mechanical deformation and the cessation of heating occur approximately simultaneously.

L'invention concerne une région d'une voilure devant être protégée contre tout givre accru, région qui est chauffée pour réduire la force du lien entre le givre et la voilure, et est déformée mécaniquement pour éliminer le givre accru une fois que le lien a été suffisamment affaibli. Le chauffage cesse avant la production de tout ruissellement d'eau important. La déformation mécanique et l'arrêt du chauffage ont lieu de manière approximativement simultanée.

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