NACELLE EQUIPPED WITH AT LEAST ONE EXCESS PRESSURE FLAP
摘要
<p>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 downstream 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.</p>
申请公布号
WO2009024461(A1)
申请公布日期
2009.02.26
申请号
WO2008EP60284
申请日期
2008.08.05
申请人
AIRCELLE;LORE, XAVIER RAYMOND YVES;SOULIER, PASCAL-MARIE PAUL MARCEL;DE SORBAY, AURELIE;LE DOCTE, THIERRY JACQUES ALBERT
发明人
LORE, XAVIER RAYMOND YVES;SOULIER, PASCAL-MARIE PAUL MARCEL;DE SORBAY, AURELIE;LE DOCTE, THIERRY JACQUES ALBERT