Turbofan with a thrust reverser provided with a fairing attached thereto in the fluid stream

摘要

In a turbofan associated with a thrust reverser, the internal structure (11) forming the turbofan primary cowl and the external structure (12) supporting said reverser (10) do not comprise any link in the lower part of the structures (11, 12) and form between them (11, 12) a ring-shaped air flow channel (15). A shroud (25) is arranged in said channel (15) on the downstream side of an arm (3) forming the external support structure of the turbojet aft fan duct external wall.