AIRCRAFT TURBOJET ENGINE THRUST REVERSER WITH A LOWER NUMBER OF ACTUATORS

摘要

This cascade-type thrust reverser with one-piece moving cowl (23) comprises rails able to slide in guideways positioned on each side of a suspension pylon (8). This thrust reverser comprises just two actuators (43a, 43b) positioned near said rails and able to cause this cowl (23) to slide on said guideways between its direct-jet and reverse-jet positions. It also comprises means capable of compensating for forces that have a tendency to misalign said rails with respect to said guideways, thus preventing them from jamming in one another.