Air inlet lip for a pod with electric defrosting

Details Air inlet lip for a pod with electric defrosting Air inlet lip for a pod with electric defrosting

B - Operations, Transporting

64

D

B64D 15/12 (2006.01) B64D 33/02 (2006.01) F02C 7/047 (2006.01)

Patent

CA 2643023

The present invention relates to a lip (4a) of an air inlet (4) of a turbojet pod (1) intended to be fastened to an air inlet downstream structure (4b) and including at least one electric heating element for defrosting, said electric heating element being fitted with at least one electrical connector able to be connected to at least one corresponding electricity supply connector of the downstream structure, characterised in that the lip breaks down into at least two identical structures (7) set end-to-end on a periphery of the air inlet.

La présente invention se rapporte à une lèvre (4a) d'une entrée d'air (4) d'une nacelle (1) de turboréacteur destinée à être rattachée à une structure aval (4b) d'entrée d'air et comprenant au moins un élément électrique chauffant de dégivrage, ledit élément électrique chauffant étant équipé d'au moins un connecteur électrique apte à être relié à au moins un connecteur d'alimentation électrique correspondant de la structure aval, caractérisée en ce que la lèvre se décompose en au moins deux structures (7) identiques mises bout à bout sur un pourtour de l'entrée d'air.

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