COUPLING SYSTEM CONNECTING AN INTERNAL STRUCTURE AND AN EXTERNAL STRUCTURE OF A JET ENGINE NACELLE

摘要

the present invention relates to a dual flow turbojet nacelledesigned to be attached to a structurean aircraft with a link pole and comprising a front section entrylook, a median section to surround a blowerfor jet engines and rear section with an internal structureintended to serve as a rear portion of the jet engine crankcasedefining an outer shell (5) of a vein (7) to flow athe secondary flow, the internal structure ofsubstantially radial extensions (61) through the vein and by whomit is linked to an inner panel (51) of the structure.by means of at least one external stiffener (110) with ageneral form in the square, characterised in that thea stiffener is also fixed in outer panel (52) of the structure.external.