FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly, to turbojet two-stage engine nacelle, aircraft power plant and aircraft incorporating said power plant. Nacelle 1 for turbojet two-stage engine 2 comprises front air intakes section 5, central section embracing engine fan 3, and rear section 7. Rear section comprises internal element 7b that makes engine rear casing. Said internal element has jointing appliances to allow attaching nacelle to pylon 12 arranged to be jointed to aircraft fixed element 13 on, at least, one part of said internal element.
EFFECT: reduced deformation of nacelle.
33 cl, 14 dwg
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