FIELD: transport.
SUBSTANCE: invention relates to turbojet engine nacelle air intake edge attached to downstream section of said air intake that comprises anti-acing electrical hearing element, and to appropriate downstream section and turbojet engine nacelle. Downstream element 4b of air intake 4 of nacelle 1 allows air intake edge 4a to attached thereto. Edge 4a comprises anti-icing electrical hearing element 14. Edge 4a consists of identical sections 7 butt-jointed together along perimeter of air intake 4. Said element 14 is furnished with connector assembly 15 secured in front web 18 of downstream element 4b. Said element 4b comprises power supply connector assembly 19 to interact with connector assembly 15 of edge 4a.
EFFECT: simplified replacement of air intake edge.
7 cl, 11 dwg
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