FIELD: aircraft engineering.
SUBSTANCE: aircraft nacelle comprises hot air discharge means 50 to communicated nacelle inner part with outer part and zone of communication between two elements, 56 whereat two elements are superimposed. Note here that every of said elements has surface making nacelle outer surface and opposite side of said communication zone. Said discharge means 50 comprises angular insert 52 made up of two parts. First part 58, 70, 88 is to be fitted between superimposed panels and comprises, at least, one extending and/or concave element. The latter allows forming the passage between said panels to communicate said nacelle first and second parts. Second part opposite one panel to be located inside at the level of communication zone for its protection against excess temperature.
EFFECT: higher efficiency anti-icing protection.
9 cl
