Connection assembly for engine nacelle stub utilized to fix engine under aerofoil of aircraft, has pin sliding inside interior secondary axle along L-shaped cross-piece for driving displacement of L-shaped foot before fitting aerofoil

摘要

The assembly has an L-shaped cross-piece (13) mounted through an interior secondary axle (12), where the cross-piece comprises an L-shaped foot (13a) forming a radial surface of a blind type crossing axle system. A pin (15) is slid inside the interior secondary axle along the L-shaped cross-piece for driving displacement of the foot of the L-shaped cross-piece before fitting an aerofoil. The axle system comprises a cross-piece (14) positioned symmetrically with respect to each other. An independent claim is also included for a method for installation of a connection assembly.