FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly, to aircraft engine nacelle with lateral opening of flaps. Nacelle 1 of turbojet engine 4 is jointed to aircraft airframe 2 by jointing strut 3 and comprises movable part (9', 9") that may be opened to allow access inside said nacelle. Said movable part may turn about axle 25 arranged perpendicular to airframe plane whereto nacelle is attached. Said axle 25 is arranged on nacelle by drive means of 20, 21 that allow inclining said axle relative to its initial position.
EFFECT: optimum opening of nacelle flaps.
11 cl, 10 dwg
