The pylon includes a rigid structure comprising a lengthwise casing (22) with two side panels connected by a series of transverse ribs (23), and two curved lateral housings (24a) towards its forward end supporting the front section of the engine and having at least one frame (28a, 46a). One of the transverse ribs (23) has two lateral extensions (52a) made in one piece with the rib that project from the lengthwise casing and are fixed to one of the lateral housing frames. The rear lateral frame (46a) has upper and lower flanges (60a, 62a), and each of the lateral extensions has sections connected to its upper flange and core.
MAT D'ACCROCHAGE DE TURBOREACTEUR POUR AERONEF
TURBINE ENGINE MOUNTING STRUCTURE FOR AIRCRAFT
AUFHÄNGUNGSSTRUKTUR FÜR EIN TRIEBWERK FÜR EIN FLUGZEUG
2018-08-08
Patent
Electronic Resource
French
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
MAT D'ACCROCHAGE POUR UN TURBOREACTEUR D'UN AERONEF COMPORTANT UNE STRUCTURE PARTICULIERE
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