ELECTRIC THRUST REVERSER SYSTEM FOR AN AIRCRAFT ENGINE NACELLE AND AIRCRAFT ENGINE NACELLE PROVIDED WITH SAME

摘要

The present disclosure provides an electric thrust reverser system for an aircraft engine nacelle, including a mechanism for actuating a thrust reverser mechanism. The actuating mechanism includes a first drive cylinder and a second drive cylinder. Each cylinder includes a mechanical connection casing, a primary lock (8) and a movable rod secured to a point connected to the associated thrust reverser mechanism. A motor-actuated drive unit is mechanically connected, via flexible shafts, to the mechanical connection casings of each drive cylinder and set in motion by the command of a control unit via an electrical connection. A tertiary lock is disposed for securing the associated thrust reverser mechanism, to a fixed structure of the nacelle.