SUSPENSION FOR A TURBINE ENGINE

摘要

A rear suspension for attaching an aeroengine (20) of longitudinal axis X to a carrier structure or mast (12) of an aircraft, the suspension including at least two clevis-forming vertical uprights (26A, 26B; 28A, 28B) supporting a respective horizontal slideway (30A, 30B) having a roller (32) freely mounted thereon that is suitable for moving in a slot (34A, 34B) in a lug (20A) arranged in a YZ plane of transverse axis Y and of vertical axis Z, in such a manner as to enable the aeroengine to move only in translation along the longitudinal axis X and in pivoting about said longitudinal axis X.

主权项

1. A suspension for suspending an aeroengine of longitudinal axis X on a carrier structure or mast of an aircraft, the suspension being characterized in that, on either side of an XZ plane containing said longitudinal axis X, it includes two pairs of vertical uprights with the two uprights in each pair forming a clevis supporting a respective horizontal slideway on which a roller is freely mounted that is suitable for moving in a slot of circularly arcuate shape in a lug arranged in a YZ plane of transverse axis Y and vertical axis Z, so as to enable said aeroengine to move only in translation along said slideway along said longitudinal axis X and in pivoting in said slot about said longitudinal axis X.