BYPASS TURBOJET THRUST REVERSER HAVING DOORS WITH INTEGRALLY STIFFENED EXTERNAL STRUCTURE

摘要

The invention concerns a bypass turbojet thrust reverser comprising pivoting doors (7) integrated in direct jet in the external wall of the fan air duct (15) and constituting flux deviating obstacles providing thrust reversal. The door (7) consists of a panel (23) forming an external structure and an internal structure (22) connected by a local structural linking zone (25), the rest of the external (23) and internal (22) structures being independent. The lock (27) maintaining the door (7) in closed position is installed in said structural zone (25).