FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly, to engine assembly, nacelle and lock system of nacelle movable fairing. Lock system 20 of turbojet engine nacelle movable fairing 8 to be jointed with aircraft pylon 4 comprises, on one side, lug 21 for connection with pylon and, on opposite side, rod 22 to be mounted on movable fairing and to be engaged with said lug when movable fairing is in closed position. Rod is arranged to translate relative to said movable fairing along in fact lengthwise axis of said fairing. Said rod makes latch to displace between closed position whereat it is engaged with lug to ensure joint between pylon and movable fairing, and open position whereat it is disengaged from lug to allow opening movable fairing.
EFFECT: reliable lock system to allow jointing fairing that may turn about axis perpendicular to engine lengthwise axis.
16 cl, 9 dwg
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