FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly, to turbojet nacelles. Claimed nacelle comprises the frond, mid and rear sections, an outer structure with at least one cowl mounted thereat and at least one first and second panels. Said first panel is mounted at the inner structure from one side of the nacelle for physical engagement with the wing element and its limitation between said cow land said wing element in the thrust reverse mode. The second panel is mounted at the inner structure from the nacelle opposite side for maximum increase in air volume released from the nacelle opposite side in the thrust reverse mode.
EFFECT: enlarged accessible surface for air volume released from the nacelle opposite side in the thrust reverse mode.
14 cl, 28 dwg
