FIELD: aircraft engineering.
SUBSTANCE: proposed nacelle 1 comprises front part 6 with air intake, medium part 7 and rear part 8 composed of two side covers 9 to be turned by power cylinder 11 and telescopic connection rod 12. First end 13, 14 of said cylinder and rod is secured on turbojet while second end 16, 17 is secured in appropriate side cover. Besides, nacelle comprises damper 19 arranged between every connection rod and said side cover. Note here that said damper is prestressed when side cover stays in operating position.
EFFECT: decreased weight and overall dimensions of telescopic rod.
7 cl, 3 dwg
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