FIELD: transport.
SUBSTANCE: turbojet engine nacelle has rear section 8 made up of two moving flap halves arranged to open on changing from operating position into servicing position when driven by power cylinder 11 and telescopic connection bar 12. Every said bar and power cylinder has first end 13, 14 secured in or on turbojet engine and second end 16, 17 secured to appropriate flap half. Nacelle 1 comprises damper 19 arranged between every said connection bar and flap half. Said damper is pre-stressed when flap half is in operating condition. Invention covers also power plant comprising nacelle, and aircraft with power plant.
EFFECT: ruled out overheating of flap halves drive motor.
9 cl, 1 dwg
