公开(公告)号：US10018152B2

公开(公告)日：2018-07-10

申请号：US14950564

申请日：2015-11-24

Applicant: AIRCELLE

Inventor： Sébastien Laurent Marie Pascal ,  Alexandre Breton

IPC: F02K1/72 ,  F02K1/60 ,  F02K1/62 ,  F02K1/70 ,  F02K3/06

CPC classification number: F02K1/72 ,  F02K1/60 ,  F02K1/62 ,  F02K1/70 ,  F02K3/06 ,  F05D2220/323 ,  F05D2250/14 ,  F05D2250/70

Abstract: A turbojet engine nacelle includes a thrust reversing device having doors that swing to brake a direct gas flow, guiding it through counter-thrust openings, and the inside of each door has, at the front, a cavity receiving a spoiler turned towards the front when this door is open. The nacelle includes a fixed structure upstream from each door supporting a deflection edge that partially covers the cavity. In particular, the fixed structure supports, on each side, counter-thrust openings, a flank disposed in the continuation of the deflection edge and extending behind the cavity, which is incorporated into a leaf of the door.