Patent ID: 8839629
Filing Date: 2014-09-23
Classification: B64D

Abstract:
1. An assembly for attaching hangers from which an aircraft propulsion unit is suspended, said propulsion unit being suspended from a structural element of the aircraft, said propulsion unit comprising a turbojet engine having a longitudinal axis, said attachment assembly comprising at least one clevis mount and a casing for attaching said hangers to said propulsion unit, characterized in that the casing comprises at least two connecting flanges, a first flange of the at least two connecting flanges placed upstream of the clevis and a second flange of the at least two connecting flanges placed downstream of the clevis, said at least two connecting flanges forming a rigid connection between the clevis mount and the casing at an outer periphery of said casing and along an axis parallel to the longitudinal axis of the turbojet engine.