FIELD: turbojet engines. SUBSTANCE: in proposed nozzle of turbojet engine convergent flaps are set into action by axially movable control ring. Divergent flaps are coupled with turnable ring through levers. Turnable ring is mounted by means of ball joint secured on outer wall of spherical part of structure. Rotation interlock system precludes rotation of spherical part around turbojet axis. EFFECT: improved reliability in operation. 8 cl, 8 dwg
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