FIELD: engines and pumps.
SUBSTANCE: invention relates to a nacelle of a turbojet engine having a rear section comprising at least one front frame (2) adapted for attachment to a fixed part of the nacelle. The rear section is provided with at least one rail or the slider (3). The slide extends substantially in the longitudinal direction of the nacelle and is configured to engage at least one corresponding rail or slider (3') of the turbojet engine strut fastener. The front frame is connected with the rail or the slider (3) of the rear section by means of at least one rotary connecting rod (7a, 7b).
EFFECT: invention allows to compensate for relative movements of the turbojet engine and a pylon, and increases the structural strength.
9 cl, 16 dwg
