A turbojet engine comprising an engine, a nacelle comprising a fan case, an intermediate case having a part forming a hub and an outer shroud radially spaced away from the hub by a secondary, or bypass, flow path and fixed to the hub via arms, in which the outer shroud is situated to the rear and in the continuity of the fan case, a fixed structure fixed to the outer shroud, a mobile assembly mounted with the ability to effect translational movement on the fixed structure, and a ramp fixed to the outer shroud and configured to direct the secondary or bypass flow to exit the outer shroud. Such a turbojet engine makes it possible to simplify assembly and among other things, makes it possible to fix the ramp directly to the outer shroud.
TURBOREACTEUR COMPORTANT UNE NACELLE EQUIPEE D'UN CARTER DE SOUFFLANTE ET D'UNE STRUCTURE FIXE
TURBINE ENGINE COMPRISING A NACELLE PROVIDED WITH A FAN COWL AND A STATIONARY STRUCTURE
TURBOTRIEBWERK, DAS EINE GONDEL UMFASST, DIE MIT EINEM GEBLÄSEGEHÄUSE UND EINER FESTEN STRUKTUR AUSGESTATTET IST
2020-07-22
Patent
Electronic Resource
French
TURBOREACTEUR COMPORTANT UNE NACELLE EQUIPEE D'UN CARTER DE SOUFFLANTE ET D'UNE STRUCTURE FIXE
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