FIELD: transport.
SUBSTANCE: thrust reverser comprises moving cowl connected with adjustable nozzle section making its extension and including revolving panel. Moving cowl can displace in direction parallel with nacelle axis and change from closed position whereat it ensures aerodynamic integrity of nacelle to open position whereat it opens the deflected flow channel in said nacelle. Nozzle section panel is arranged to turn to position whereat nozzle compartment cross-section is varied and to position whereat said panel shuts off the cold flow circuit. Moving cowl and panel are connected with their translation and rotation drives, respectively. Said drives are connected with panel front end via drive bar that can displace around attachment points at nozzle compartment panel and drives connected thereto. Another invention of this set relates to bypass turbojet nacelle with rear section equipped with said thrust reverser.
EFFECT: position of axes of drives parallel with nacelle axis irrespective of moving cowl and nozzle compartment panels position.
14 cl, 17 dwg
