Invention Grant
US08529196B2 Nacelle equipped with at least one excess pressure flap 有权
机舱配备至少一个多余的压力皮瓣

Nacelle equipped with at least one excess pressure flap
Abstract:
The present invention relates to a jet engine nacelle (1), of the type comprising an aft section forming an external structure (2) which, together with a concentric internal structure (4) comprising an internal panel (10) intended to surround a down-stream portion of the jet engine, defines an annular flow duct for a so-called secondary stream (3), characterized in that exhaust means (11) are formed in the internal panel such that any unwanted excess pressure is discharged into the annular duct.
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