| abstract |
The invention relates to a link assembly of a reactor mast under an aircraft wing, the wing having a fitting (6), the reactor mast having a yoke (5) fitted into the fitting and fixed to said fitting by means of a traversing axle system (10), comprising: an external main axis (11), a secondary axis (12) mounted inside the main axis, a main shoulder (13) mounted directly around the main axis, at a blind end of the axis system, for locking said axis in translation, a secondary shoulder (14) mounted around one end of the secondary axis, at a blind end of the axis system, for locking the rotating system, - a locking assembly (15, 16) mounted around the main axis and the secondary axis, at a free end of the axis system, for locking the translation axis system. |