公开(公告)号：US12292015B2

公开(公告)日：2025-05-06

申请号：US18644977

申请日：2024-04-24

Applicant: Airbus Operations SAS

Inventor： Frédéric Chelin ,  Christophe Bourdeau ,  Olivier Scholz

IPC: F02K1/72 ,  F02K1/62 ,  F02K1/76

Abstract: An aircraft nacelle equipped with a thrust reversal device which comprises: at least one deflection system configured to deflect an air stream channeled in the nacelle toward a lateral opening of the nacelle, in the activated state; at least one orientation system having: at least one transverse deflector configured to orient the air stream deflected by the deflection system toward the upstream end of the nacelle, at least one downstream deflector positioned at the downstream edge of the lateral opening and configured to deflect the air stream deflected by the deflection system toward the upstream end of the nacelle.