SEITLICH ÖFFNENDE TRIEBWERKSGONDEL

摘要

The nacelle has movable cowls (3) articulated to an longitudinal axis of the nacelle to open the cowls for providing access to a two-flow turbojet (1), and paired by an attachment unit (8) which permits articulation of the cowls one on another around a discrete or merged hinge line (6). Each cowl has a permanent connection unit constituted of a hanger and a support rod or a temporary link unit to provide temporary link when the cowl is close in rotation with a fan casing (7) of the nacelle. The link unit has a recess cut out (15) to receive a stop (14) arranged in a peripheral groove (13).