Jet engine thrust reverser door equiped with an auxiliary flap.

摘要

The present invention relates to door-type thrust reversers for aircraft jet engines. The door (2) is equipped, on the internal face of its upstream end, with at least one auxiliary flap (8) articulated to the door and capable of being brought from a position remote from the internal face of the door into a position against the latter, and locked in each one of these positions by virtue of an operating device with linkages (12, 17, 21, 19). The operating device is actuated by virtue of its interaction with a fixed limit stop (23). Locking the flap (8) in each one of its positions avoids vibration thereof and damage thereto. <IMAGE>