Patent ID: 8662440
Filing Date: 2014-03-04
Classification: A61P,B64D

Abstract:
1. An aft pylon fairing for a suspension system for an engine, designed to be inserted between an aircraft wing and said engine, said fairing forming a box and comprising: two side panels assembled to each other by inner cross stiffening ribs spaced at intervals from each other along a longitudinal direction of said fairing; a heat protection deck provided with an outer surface designed to delimit a core engine flow of said engine, said heat protection deck having two opposite side ends; and two longitudinal connecting walls offsetting said heat protection deck from said inner cross stiffening ribs, each of said two longitudinal walls having a first side end fixed to one or the other of the two side ends of said heat protection deck, and a second side end rigidly fixed to said inner cross stiffening ribs.