THRUST REVERSER HAVING A LOCKABLE VARIABLE NOZZLE SECTION

摘要

The present invention relates to a thrust reverser (1) including at least one translatably movable cowl (3, 4) capable of alternately shifting between a closed position in which same ensures the aerodynamic continuity of the nacelle and which covers the deflecting means, and an open position in which same opens a passage in the nacelle and uncovers the deflecting means, said thrust reverser likewise including at least one variable nozzle section (3, 3a) arranged in the extension of the movable thrust-reversing cowl (4) and provided with at least one locking means (201) capable of engaging with a complementary locking means (202) of the movable reversing cowl so as to optionally mechanically link the movable nozzle section to the movable reversing cowl.