Patent ID: 9587583
Date: 2017-03-07
CPC Classifications: F02K,Y02T

Claim:
1. A turbojet engine nacelle, comprising a thrust reverser device and an actuating system for said thrust reverser device, said thrust reverser device comprising: at least one moving cowl mounted translatably in a direction substantially parallel to a longitudinal axis of the nacelle alternating between a closed position, in which said moving cowl provides the aerodynamic continuity of the nacelle, and an open position, in which said moving cowl opens a passage in the nacelle for a deflected flow, the moving cowl comprising multiple reverser flaps; and at least one jet nozzle section for gases that extends said moving cowl and includes at least one nozzle flap mounted movable between a closed position and at least one open position in which said nozzle flap opens a leakage passage toward the outside of the nozzle section, wherein the nozzle flap is mounted pivoting on the moving cowl, and the actuating system comprises actuating means shared with the moving cowl and the nozzle flap and activates the translational movement of the moving cowl and the pivoting of the nozzle flap between three following positions: