FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly, to power plant with aircraft suspension and engine nacelle rear section. Proposed power plant comprises aircraft bypass turbojet engine and nacelle secured on intermediate crankcase to confine annular space for secondary flow around turbojet engine. Said nacelle has rigid cylindrical section and annular flange arranged on its front end to be secured on 180° of outer surface of intermediate flange. Note here that cylindrical supporting and guiding rear crankcase of turbojet engine on rear end also comprises means of fastening engine suspension elements to aircraft engine parts 22.
EFFECT: simplified attachment of aircraft engine and smaller side of its nacelle.
19 cl, 7 dwg
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