公开(公告)号：US20250109723A1

公开(公告)日：2025-04-03

申请号：US18726923

申请日：2023-01-06

Applicant: SAFRAN NACELLES

Inventor： Gina FERRIER ,  Patrick GONIDEC ,  Loïc CHAPELAIN (Deceased) ,  Edouard Marie Gabriel RAMSTEIN ,  Patrick André BOILEAU

IPC: F02K1/72

Abstract: A thrust reverser for an aircraft propulsion assembly, including at least one sealing membrane designed to deflect at least one portion of the secondary flow towards a set of cascades when the movable structure of the reverser is in the retracted thrust reversal position, the reverser also including a first flexible hook connecting a first end of the membrane to the fixed structure of the reverser, a second hook connecting a second end of the membrane to the fixed structure or to the movable structure, the second hook being fixed to the radially inner delimiting wall of the secondary vein, or guided by an internal guide fixed to the same radially inner delimiting wall.