Rotable exhaust nozzle for an aircraft engine

摘要

The nozzle has an upstream end (12) with two cylindrical pivots (22) diametrically opposite and exterior to the nozzle. Each pivot is connected to a conduit (16) of an engine of an aircraft by an elastically deformable mono block articulation unit (24) with small dimensions. A displacement unit has an actuator mounted to the exterior of the nozzle on the conduit, where the rotation of the nozzle occurs in two directions around a transversal axis which is the yaw axis of the aircraft and is controlled by the actuator.