Method of de-icing the leading edge of an aerodynamic...

Details Method of de-icing the leading edge of an aerodynamic... Method of de-icing the leading edge of an aerodynamic...

B - Operations, Transporting

64

D

B64D 15/04 (2006.01) B64C 21/10 (2006.01)

Patent

CA 2632873

According to the invention, on at least one of the faces (1E, 1I) of said leading edge (1), forward of the partition (3), an action is exerted on the fluid flow (EF) so as to cause the latter to switch from the laminar state (EFL) to the turbulent state (EFT) in order to increase the thermal exchanges and minimize the thermal stresses on said leading edge.

Selon l'invention, sur au moins l'une des faces (1 E, 1I) dudit bord d'attaque (1), en avant de la cloison (3), on exerce une action sur l'écoulement fluide (EF) pour faire passer celui-ci de l'état laminaire (EFL) à l'état turbulent (EFT) afin d'augmenter les échanges thermiques et minimiser les contraintes thermiques sur ledit bord d'attaque.

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