Invention Grant
US08845287B2 Turbojet engine nacelle 有权
涡轮喷气发动机舱

Turbojet engine nacelle
Abstract:
A nacelle for a turbojet engine is provided that includes an air intake upstream from the turbojet engine, a middle section intended to surround a fan of the turbojet engine and its case, and a downstream section. The middle section is made from at least one aerostructure capable of ensuring external aerodynamic continuity of the nacelle, and the aerostructure is rigidly bound, so as to be able to be taken apart, to at least one surrounding fixed structure.
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