FIELD: transportation.
SUBSTANCE: invention relates to aviation, in particular to aircraft engine nacelles. The aircraft engine nacelle contains the static front frame, the thrust reverser cowl, the thrust reverser power cylinders, the variable geometry nozzle, driving and transmission shafts. The thrust reverser cowl is installed with a possibility of sliding with reference to the front frame between the positions of direct and reverse thrust. The driving shafts are installed with a possibility of separation of transmission shafts when moving the cowl downstream into the position of reverse thrust.
EFFECT: decrease of weight of nacelle units is achieved.
4 cl, 5 dwg
