FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, namely, to turbojet aircraft nacelle. Proposed nacelle comprises front section with air intake 1, centre section 2 enclosing turbojet blower, and rear section 3 formed by first and second side covers 11, 12. Every side cover may be turned between working position whereat covers are jointed together and servicing position whereat they are disjointed. First side cover 11 is furnished with first follower 19 arranged at a distance from axis of rotation. Note here that first follower 19 serves to rest on first guide element 28 in turn of first side cover relative to turbojet engine. Besides, first side cover 11 is provided with second follower 20 arranged at angle to first follower 19 relative to axis of rotation A of first side cover 11 to rest on second guide element 29 in turn of first side cover.
EFFECT: decreased overall dimensions.
11 cl, 7 dwg
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