TURBOJET THRUST REVERSER WITH INTERNAL BUCKETS

摘要

The invention concerns a turbojet thrust reverser comprising a mobile part consisting of two internal buckets (12) mounted on fixed pivots (18) of the fixed structure (1) and an axially mobile annular structure (11) constituting the pod downstream external part (13) and in direct jet, the downstream part (15) of the airstream channel radially external wall, forming the trailing edge and covering said buckets (12) which constitute part of said airstream radially external wall.