FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, namely, to turbojet nacelle. Turbojet nacelle comprises air intake front part 1, medium part 2 and rear part 3 made up of two lateral covers 9, 10 fitted to turn about axle A. Medium part 2 and rear part 3 are jointed together by frame 12 secured relative to turbojet. Note here that first and second side covers 9, 10 are equipped with mounts 13 interacting with mate mounts 14 arranged at frame 12. Lateral cover 10 is provided with retainers 20 interacting with mate retainers 16, 17 arranged at the frame to prevent displacement of lateral cover 10 at axle A. Note here that retainer comprises slot 17 made at frame 12 or vice versa.
EFFECT: better protection of nacelle in servicing.
8 cl, 6 dwg
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RU2460673C2 |
