FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly, to turbojet nacelles. Turbojet engine nacelle comprises the blower casing, front frame, flow deflector, thrust reverser and reinforcing structure. The front frame can be mounted behind said blower casing to interact with the thrust reverser cowl and to support at least one flow deflector. Said thrust reverser can slide from closed position to overlap the flow deflector to open position to release the flow deflector. Reinforcing structure is located along the nacelle lengthwise axis to allow mounting thereat of the third protection line and/or retainer between the front frame and the thrust reverser cowl.
EFFECT: higher reliability and safety.
15 cl, 9 dwg
