FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly, to aircraft power plant and engine cylindrical nacelle. Proposed power plant comprises bypass turbojet engine and engine nacelle 10 secured on engine intermediate casing to define annular space for gas secondary flow around said engine. Nacelle comprises downstream structure 16 made up of two sections. One of the latter makes stationary frame 26 comprising fasteners 20 of engine suspension components 22, 24 to secure them to aircraft part 18 and those to secure to engine intermediate casing. Another section is a moving part 40 arranged on stationary frame 26 to displace between working position and opening position.
EFFECT: decreased overall dimensions of power plant and nacelle.
11 cl, 5 dwg
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